Subject: (05) Aircraft Design, Testing And Performance
Number of records: 344.
Whitmore, Stephen A. and Moes, Timothy R. (1999) A Base Drag Reduction Experiment on the X-33 Linear Aerospike SR-71 Experiment (LASRE) Flight Program. Technical Report NASA/TM-1999-206575, Research Engineering, NASA Dryden Flight Research Center.
Whitmore, Stephen A. and Moes, Timothy R. (1999) A Base Drag Reduction Experiment on the X-33 Linear Aerospike SR-71 Experiment (LASRE) Flight Program. Meeting Paper AIAA-1999-0277, Research Engineering, NASA Dryden Flight Research Center.
Larson, Terry J. and Ehernberger, L.J. (1985) A Constant Altitude Flight Survey Method for Mapping Atmospheric Ambient Pressures and Systematic Radar Errors. Technical Report NASA TM-86733, Research Engineering, NASA Dryden Flight Research Center.
Cox, T. and Sachs, G. and Knoll, A. and Stich, R. (1995) A Flying Qualities Study of Longitudinal Long-Term Dynamics of Hypersonic Planes. Technical Report NASA TM-104308, Research Engineering, NASA Dryden Flight Research Center.
Cotting, M. Christopher and Cox, Timothy H. (2005) A Generic Guidance and Control Structure for Six-Degree-of-Freedom Conceptual Aircraft Design. Technical Report NASA/TM-2005-212866, Research Engineering, NASA Dryden Flight Research Center.
Cotting, M. Christopher and Cox, Timothy H. (2005) A Generic Guidance and Control Structure for Six-Degree-of-Freedom Conceptual Aircraft Design. Meeting Presentation AIAA-2005-0032, Research Engineering, NASA Dryden Flight Research Center.
Cox, Timothy H. and Cotting, M. Christopher (2005) A Generic Inner-Loop Control Law Structure for Six-Degree-of-Freedom Conceptual Aircraft Design. Technical Report NASA/TM-2005-212865, Research Engineering, NASA Dryden Flight Research Center.
Kehoe, Michael W. (1995) A Historical Overview of Flight Flutter Testing. Technical Report NASA TM-4720, Research Engineering, NASA Dryden Flight Research Center.
Kehoe, Michael W. (1995) A Historical Overview of Flight Flutter Testing. Conference Paper AGARD-CP-566, Paper No. 1, Research Engineering, NASA Dryden Flight Research Center.
Carter, John F. and Nagy, Christopher J. and Barnicki, Joseph S. (1997) A Model for Space Shuttle Orbiter Tire Side Forces Based on NASA Landing Systems Research Aircraft Test Results. Technical Report NASA TM-4808, Research Engineering, NASA Dryden Flight Research Center.
Tang, Ming H. and Sheldon, Robert G. (1980) A Modified T-Value Method for Selection of Strain Gages for Measuring Loads on a Low Aspect Ratio Wing. Technical Report NASA Technical Paper TP-1748, Research Engineering, NASA Dryden Flight Research Center.
Powers, Bruce G. (1966) A Parametric Study of Factors Influencing the Deep-Stall Pitch-Up Characteristics of T-Tail Transport Aircraft. Technical Report NASA Technical Note TN D-3370, Research Engineering, NASA Dryden Flight Research Center.
Burcham Jr., F.W. and Fullerton, C. Gordon and Gilyard, Glenn B. and Wolf, Thomas D. and Stewart, James F. (1991) A Preliminary Investigation of the Use of Throttles for Emergency Flight Control. Technical Report NASA TM-4320, Research Engineering, NASA Dryden Flight Research Center.
Whitmore, Stephen A. and Hurtado, Marco and Rivera, Jose and Naughton, Jonathan W. (2000) A Real-Time Method for Estimating Viscous Forebody Drag Coefficients. Technical Report NASA/TM-2000-209015, Research Engineering, NASA Dryden Flight Research Center.
Whitmore, Stephen A. and Hurtado, Marco and Rivera, Jose and Naughton, Jonathan W. (2000) A Real-Time Method for Estimating Viscous Forebody Drag Coefficients. Meeting Paper AIAA-2000-0781, Research Engineering, NASA Dryden Flight Research Center.
Layton, Garrison P. (1984) A Review of Recent Developments in Flight Test Techniques at the Ames Research Center, Dryden Flight Research Facility. Technical Report NASA TM-86039, Research Engineering, NASA Dryden Flight Research Center.
Ehernberger, L. J. and Donohue, Casey and Teets Jr., Edward H. (2004) A Review of Solar-Powered Aircraft Flight Activity at the Pacific Missile Range Test Facility, Kauai, Hawaii. Meeting Paper AMS P8.3, Research Engineering, NASA Dryden Flight Research Center.
Powers, Bruce G. (1968) A Review of Transport Handling-Qualities Criteria in Terms of Preliminary XB-70 Flight Experience. Technical Report NASA TM X-1584, Research Engineering, NASA Dryden Flight Research Center.
Johnson, Steven A. (1990) A Simple Dynamic Engine Model for Use in a Real-Time Aircraft Simulation With Thrust Vectoring. Technical Report NASA TM-4240, Research Engineering, NASA Dryden Flight Research Center.
Martin, C. Wayne and Breiner, David M. (2004) A Six-Node Curved Triangular Element and a Four-Node Quadrilateral Element for Analysis of Laminated Composite Aerospace Structures. Technical Report NASA/CR-2004-210725, Research Engineering, NASA Dryden Flight Research Center.
Richwine, David M. and Curry, Robert E. and Tracy, Gene V. (1989) A Smoke Generator System for Aerodynamic Flight Research. Technical Report NASA TM-4137, Research Engineering, NASA Dryden Flight Research Center.
Banner, Richard D. and Kuhl, Albert E. (1966) A Summary of X-15 Heat-Transfer and Skin-Friction Measurements. Technical Report NASA TM X-1210, Research Engineering, NASA Dryden Flight Research Center.
Lind, Rick C. and Brenner, Martin J. (1998) A Worst-Case Approach for On-Line Flutter Prediction. Technical Report NASA/TM-1997-207056, Research Engineering, NASA Dryden Flight Research Center.
Brenner, Martin J. (1993) Actuator and Aerodynamic Modeling for High-Angle-of-Attack Aeroservoelasticity. Technical Report NASA TM-4493, Research Engineering, NASA Dryden Flight Research Center.
Gupta, K.K. and Doyle, T. and Hahn, E. (2005) AE/Flutter Simulation and Flight Test Correlation of the F/A-18 Active Aeroelastic Wing (AAW). Meeting Presentation AIAA-2005-233, Research Engineering, NASA Dryden Flight Research Center.
Noffz, Gregory K. and Moes, Timothy R. and Haering Jr., Edward A. and Kolodziej, Paul (1992) Aerothermal Test Results From the Second Flight of the Pegasus® Booster. Technical Report NASA TM-4391, Research Engineering, NASA Dryden Flight Research Center.
Larson, Richard R. (1987) AFTI/F-111 MAW Flight Control System and Redundacy Management Description. Technical Report NASA TM-88267, Research Engineering, NASA Dryden Flight Research Center.
Kehoe, Michael W. (1988) Aircraft Flight Flutter Testing at the NASA Ames-Dryden Flight Research Facility. Technical Report NASA TM-100417, Research Engineering, NASA Dryden Flight Research Center.
Johnson, Steven A. (1992) Aircraft Ground Test and Subscale Model Results of Axial Thrust Loss Caused by Thrust Vectoring Using Turning Vanes. Technical Report NASA TM-4341, Research Engineering, NASA Dryden Flight Research Center.
Kehoe, Michael W. (1987) Aircraft Ground Vibration Testing at NASA Ames-Dryden Flight Research Facility. Technical Report NASA TM-88272, Research Engineering, NASA Dryden Flight Research Center.
Kehoe, Michael W. and Freudinger, Lawrence C. (1994) Aircraft Ground Vibration Testing at the NASA Dryden Research Facility – 1993. Technical Report NASA TM-104275, Research Engineering, NASA Dryden Flight Research Center.
Iliff, Kenneth W. (1987) Aircraft Parameter Estimation- AIAA Dryden Lecture in Research for 1987. Technical Report NASA TM-88281, Research Engineering, NASA Dryden Flight Research Center.
Haering Jr., Edward A. (1990) Airdata Calibration of a High-Performance Aircraft for Measuring Atmospheric Wind Profiles. Technical Report NASA TM-101714, Research Engineering, NASA Dryden Flight Research Center.
Haering Jr., Edward A. (1995) Airdata Measurement and Calibration. Technical Report NASA TM-104316, Research Engineering, NASA Dryden Flight Research Center.
Brumbaugh, Randal W. (1991) An Aircraft Model for the AIAA Controls Design Challenge. Technical Report NASA CR-186019, Research Engineering, NASA Dryden Flight Research Center.
Taylor Jr., Lawrence W. and Smith, John W. (1967) An Analysis of the Limit-Cycle and Structural-Resonance Characteristics of the X-15 Stability Augmentation System. Technical Report NASA Technical Note TN D-4287, Research Engineering, NASA Dryden Flight Research Center.
Powers, Sheryll Goecke (1995) An Electronic Workshop on the Performance Seeking Control and Propulsion Controlled Aircraft Results of the F-15 Highly Integrated Digital Electronic Control Flight Research Program: Proceedings of the Electronic Workshop. Technical Report NASA/TM-104278, Research Engineering, NASA Dryden Flight Research Center.
Duke, Eugene L. and Regenie, Victoria A. and Brazee, Marylouise and Brumbaugh, Randal W. (1986) An Engineering Approach to the Use of Expert Systems Technology in Avionics Applications. Technical Report NASA TM-88263, Research Engineering, NASA Dryden Flight Research Center.
Barber, Marvin R. and Jones, Charles K. and Sisk, Thomas R. and Haise, Fred W. (1966) An Evaluation of the Handling Qualities of Seven General-Aviation Aircraft. Technical Report NASA Technical Note TN D-3726, Research Engineering, NASA Dryden Flight Research Center.
Olney, Candida D. and Hillebrandt, Heather and Reichenbach, Eric Y. (2000) An Evaluation Technique for an F/A-18 Aircraft Loads Model Using F/A-18 Systems Research Aircraft Flight Data. Technical Report NASA/TM-2000-209028, Research Engineering, NASA Dryden Flight Research Center.
Kehoe, Michael W. and Laurie, Edward J. and Bjarke, Lisa J. (1990) An In-Flight Interaction of the X-29A Canard and Flight Control System. Technical Report NASA TM-101718, Research Engineering, NASA Dryden Flight Research Center.
Bjarke, Lisa J. and Ehernberger, L. J. (1989) An In-Flight Technique for Wind Measurement in Support of the Space Shuttle Program. Technical Report NASA TM-4154, Research Engineering, NASA Dryden Flight Research Center.
Murray, James E. and Bowers, Albion H. and Lokos, William A. and Peters, Todd L. and Gera, Joseph (1998) An Overview of an Experimental Demonstration Aerotow Program. Technical Report NASA/TM-1998-206566, Research Engineering, NASA Dryden Flight Research Center.
Pahle, Joseph W. and Wichman, Keith D. and Foster, John V. and Bundick, W. Thomas (1996) An Overview of Controls and Flying Qualities Technology on the
F/A-18 High Alpha Research Vehicle. In Proceedings High-Angle-of-Attack Technology Conference, pages 193-219, NASA Langley Research Center, Hampton, Virginia.
Burcham Jr., Frank W. and Gatlin, Donald and Stewart, James F. (1995) An Overview of Integrated Flight-Propulsion Controls Flight Research on the NASA F-15 Research Airplane. Electronic Workshop Presentation, Research Engineering, NASA Dryden Flight Research Center.
Bowers, Albion H. and Pahle, Joseph W. and Wilson, R. Joseph and Flick, Bradley C. and Rood, Richard L. (1996) An Overview of the NASA F-18 High Alpha Research Vehicle. Technical Report NASA TM-4772, Research Engineering, NASA Dryden Flight Research Center.
Wolowicz, Chester H. (1966) Analysis of an Emergency Deceleration and Descent of the XB-70-1 Airplane due to Engine Damage Resulting from Structural Failure. Technical Report NASA TM X-1195, Research Engineering, NASA Dryden Flight Research Center.
Freudinger, Lawrence C. (1991) Analysis of Structural Response Data Using Discrete Modal Filters. Technical Report NASA CR-179448, Research Engineering, NASA Dryden Flight Research Center.
Carr, Peter C. and McKissick, Burnell T. (1988) Analysis Procedures and Subjective Flight Results of a Simulator Validation and Cue Fidelity Experiment. Technical Report NASA TM-88270, Research Engineering, NASA Dryden Flight Research Center.
Washington, Harold P. and Gibbons, John T. (1973) Analytical Study of Takeoff and Landing Performance for a Jet STOL Transport Configuration with Full-Span, Externally Blown, Triple-Slotted Flaps. Technical Report NASA Technical Note TN D-7441, Research Engineering, NASA Dryden Flight Research Center.
Redin, Paul C. (1981) Application of a Performance Modeling Technique to an Airplane with Variable Sweep Wings. Technical Report NASA TP-1855, Research Engineering, NASA Dryden Flight Research Center.
Maine, Richard E. and Iliff, Kenneth W. (1986) Application of Parameter Estimation to Aircraft Stability and Control – The Output-Error Approach. Technical Report NASA Reference Publication RP-1168, Research Engineering, NASA Dryden Flight Research Center.
Maine, Richard E. and Murray, James E. (1986) Application of Parameter Estimation to Highly Unstable Aircraft. Technical Report NASA TM-88266, Research Engineering, NASA Dryden Flight Research Center.
Hewett, M.D. and Tartt, D.M. and Agarwal, A. (1991) Automated Flight Test Management System. Technical Report NASA CR-186011, Research Engineering, NASA Dryden Flight Research Center.
Larson, Richard R. (1999) Automated Testing Experience of the Linear Aerospike SR-71 Experiment (LASRE) Controller. Technical Report NASA/TM-1999-206588, Research Engineering, NASA Dryden Flight Research Center.
Dibley, Ryan P. and Allen, Michael J. and Nabaa, Dr. Nassib (2007) Autonomous Airborne Refueling Demonstration, Phase I Flight-Test Results. Technical Report NASA/TM-2007-214632, Research and Engineering, NASA Dryden Flight Research Center.
Burcham Jr., Frank W. (1995) Background and Principles of Throttles-Only Flight Control. Electronic Workshop Presentation, Research Engineering, NASA Dryden Flight Research Center.
Saltzman, Edwin J. and Goecke, Sheryll A. and Pembo, Chris (1968) Base Pressure Measurements on the XB-70 Airplane at Mach Numbers from 0.4 to 3.0. Technical Report NASA TM X-1612, Research Engineering, NASA Dryden Flight Research Center.
Whitmore, Stephen A. and Moes, Timothy R. (2000) Base-Drag-Reduction Experiments on the X-33 Linear Aerospike SR-71 Flight Program. Journal of Spacecraft and Rockets 37(3):297-303.
Iliff, Kenneth W. and Maine, Richard E. (1986) Bibliography for Aircraft Parameter Estimation. Technical Report NASA TM-86804, Research Engineering, NASA Dryden Flight Research Center.
Voracek, David F. and Clarke, Robert (1991) Buffet Induced Structural/Flight-Control System Interaction of the X-29A Arcraft. Technical Report NASA TM-101735, Research Engineering, NASA Dryden Flight Research Center.
Herrera, Claudia Y. and Pak, Chan-gi (2007) Build-up Approach to Updating the Mock Quiet Spike™ Beam Model. Technical Report NASA/TM-2007-214621, Research Engineering, NASA Dryden Flight Research Center.
Herrera, Claudia Y. and Pak, Chan-gi (2007) Build-up Approach to Updating the Mock Quiet Spike™ Beam Model. Meeting Paper AIAA-2007-1776, Research Engineering, NASA Dryden Flight Research Center.
Vachon, Michael Jacob and Ray, Ronald J. and Calianno, Carl (2004) Calculated Drag of an Aerial Refueling Assembly Through Airplane Performance Analysis. Technical Report NASA/TM-2004-212043, Research Engineering, NASA Dryden Flight Research Center.
Vachon, Michael Jacob and Ray, Ronald J. and Calianno, Carl (2004) Calculated Drag of an Aerial Refueling Assembly Through Airplane Performance Analysis. Meeting Paper AIAA-2004-381, Research Engineering, NASA Dryden Flight Research Center.
Hicks, John W. and Kania, Jan and Pearce, Robert and Mills, Glen (1987) Challenges in Modeling the X-29 Flight Test Performance. Technical Report NASA TM-88282, Research Engineering, NASA Dryden Flight Research Center.
Putnam, Terrill W. and Robinson, M. R. (1984) Closing the Design Loop on HiMAT (High Maneuverable Aircraft Technology). Technical Report NASA TM-85923, Research Engineering, NASA Dryden Flight Research Center.
Quinn, Robert D. and Fields, Roger A. (1986) Comparison of Measured and Calculated Temperatures for a Mach 8 Hypersonic Wing Test Structure. Technical Report NASA TM-85918, Research Engineering, NASA Dryden Flight Research Center.
Hughes, Donald L. (1981) Comparison of Three Thrust Calculation Methods Using In-Flight Thrust Data. Technical Report NASA TM-81360, Research Engineering, NASA Dryden Flight Research Center.
Goecke, Sheryll A. (1971) Comparison of Wind-Tunnel and Flight-Measured Base Pressures from the Sharp-Leading-Edge Upper Vertical Fin of the X-15 Airplane for Turbulent Flow at Mach Numbers from 1.5 to 5.0. Technical Report NASA Technical Note TN D-6348, Research Engineering, NASA Dryden Flight Research Center.
Cobleigh, Brent R. and Croom, Mark A. (2001) Comparison of X-31 Flight and Ground-Based Yawing Moment Asymmetries at High Angles of Attack. Technical Report NASA/TM-2001-210393, Research Engineering, NASA Dryden Flight Research Center.
Whitmore, Stephen A. and Leondes, Cornelius T. (1990) Compensating for Pneumatic Distortion in Pressure Sensing Devices. Technical Report NASA TM-101716, Research Engineering, NASA Dryden Flight Research Center.
Stachowiak, Susan J. and Cobleigh, Brent R. and Maliska, Heather A. and Mizukami, Masashi and Whitmore, Stephen A. and Cox, Timothy H. (2006) Conceptual Design Study for an X-38 Transonic Rocket Assist Configuration. Technical Report NASA/TP-2006-213672, Research Engineering, NASA Dryden Flight Research Center.
Fisher, David F. and Cobleigh, Brent R. (1994) Controlling Forebody Asymmetries in Flight—Experience With Boundary Layer Transition Strips. Technical Report NASA TM-4595, Research Engineering, NASA Dryden Flight Research Center.
Schweikhard, William G. and Berry, Donald T. (1974) Cooperative Airframe/Propulsion Control for Supersonic Cruise Aircraft. Meeting Paper SAE 740478, Research Engineering, NASA Dryden Flight Research Center.
Kehoe, Michael W. and Deaton, Vivian C. (1993) Correlation of Analytical and Experimental Hot Structure Vibration Results. Technical Report NASA TM-104269, Research Engineering, NASA Dryden Flight Research Center.
Weil, Joseph and Day, Richard E. (1956) Correlation of Flight and Analog Investigations of Roll Coupling. Technical Report NACA RM H56F08, Research Engineering, NASA Dryden Flight Research Center.
Schuster, Lawrence S. and Lokos, William A. (1988) Current Flight Test Experience Related to Structural Divergence of Forward-Swept Wings. Technical Report NASA TM-100445, Research Engineering, NASA Dryden Flight Research Center.
Lizotte, Andrew M. and Lokos, William A. (2005) Deflection-Based Aircraft Structural Loads Estimation With Comparison to Flight. Meeting Presentation AIAA-2005-2016, Research Engineering, NASA Dryden Flight Research Center.
Lizotte, Andrew M. and Lokos, William A. (2005) Deflection-Based Structural Loads Estimation From the Active Aeroelastic Wing F/A-18 Aircraft. Technical Report NASA/TM-2005-212871, Research Engineering, NASA Dryden Flight Research Center.
Duke, Eugene L. and Regenie, Victoria A. (1985) Description of an Experimental Expert System Flight Status Monitor. Technical Report NASA TM-86791, Research Engineering, NASA Dryden Flight Research Center.
Monaghan, Richard C. (1981) Description of the HiMAT Tailored Composite Structure and Laboratory Measured Vehicle Shape Under Load. Technical Report NASA TM-81354, Research Engineering, NASA Dryden Flight Research Center.
Corda, Stephen and Vachon, Michael Jacob (2006) Design and Flight Evaluation of a New Force-Based Flow Angle Probe. Technical Report NASA/TM-2006-213673, Research Engineering, NASA Dryden Flight Research Center.
Glover, Richard D. (1987) Design and Initial Application of the Extended Aircraft Interrogation and Display System - Multiprocessing Ground Support Equipment for Digital Flight Systems. Technical Report NASA TM-86740, Research Engineering, NASA Dryden Flight Research Center.
Flick, Bradley C. and Thomson, Michael P. and Regenie, Victoria A. and Wichman, Keith D. and Pahle, Joseph W. and Earls, Michael R. (1996) Design and Integration of an Actuated Nose Strake Control System. Technical Report NASA TM-104324, Research Engineering, NASA Dryden Flight Research Center.
Maine, Trindel A. and Burcham Jr., Frank W. and Schaefer, Peter and Burken, John (1995) Design Challenges Encountered in the F-15 PCA Flight Test Program. Electronic Workshop Presentation, Research Engineering, NASA Dryden Flight Research Center.
Lokos, William A. and Bahm, Catherine M. and Heinle, Robert A. (1994) Determination of Stores Pointing Error Due to Wing Flexibility Under Flight Load. Technical Report NASA TM-4646, Research Engineering, NASA Dryden Flight Research Center.
Snyder, H. Todd and Kehoe, Michael W. (1991) Determination of the Effects of Heating on Modal Characteristics of an Aluminum Plate With Application to Hypersonic Vehicles. Technical Report NASA TM-4274, Research Engineering, NASA Dryden Flight Research Center.
Kempel, Robert W. and Painter, Weneth D. and Thompson, Milton O. (1994) Developing and Flight Testing the HL-10 Lifting Body: A Precursor to the Space Shuttle. Technical Report NASA Reference Publication RP-1332, Research Engineering, NASA Dryden Flight Research Center.
Potter, Starr and Lind, Rick (2001) Developing Uncertainty Models for Robust Flutter Analysis Using Ground Vibration Test Data. Technical Report NASA/TM-2001-210392, Research Engineering, NASA Dryden Flight Research Center.
Potter, Starr and Lind, Rick (2001) Developing Uncertainty Models for Robust Flutter Analysis Using Ground Vibration Test Data. Meeting Paper AIAA-2001-1585, Research Engineering, NASA Dryden Flight Research Center.
Burcham Jr., Frank W. and Maine, Trindel A. and Fullerton, C. Gordon and Webb, Lannie Dean (1996) Development and Flight Evaluation of an Emergency Digital Flight Control System Using Only Engine Thrust on an F-15 Airplane. Technical Report NASA TP-3627, Research Engineering, NASA Dryden Flight Research Center.
Duke, Eugene L. and Jones, Frank P. and Roncoli, Ralph B. (1986) Development and Flight Test of an Experimental Maneuver Autopilot for a Highly Maneuverable Aircraft. Technical Report NASA TP-2618, Research Engineering, NASA Dryden Flight Research Center.
Whitmore, Stephen A. and Cobleigh, Brent R. and Jacobson, Steven R. and Jensen, Steven C. and Hennings, Elsa J. (2004) Development and Testing of a Drogue Parachute System for X-37 ALTV/B-52H Separation. Technical Report NASA/TM-2004-212044, Research Engineering, NASA Dryden Flight Research Center.
Whitmore, Stephen A. and Cobleigh, Brent R. and Jacobson, Steven R. and Jensen, Steven C. and Hennings, Elsa J. (2004) Development and Testing of a Drogue Parachute System For X-37 ALTV/B-52H Separation. Meeting Paper AIAA-2004-873, Research Engineering, NASA Dryden Flight Research Center.
Orme, John S. and DeLaat, John C. and Southwick, Robert D. and Gallops, George W. and Doane, Paul M. (1998) Development and Testing of a High Stability Engine Control (HISTEC) System. Technical Report NASA/TM-1998-206562, Research Engineering, NASA Dryden Flight Research Center.
Dibley, Ryan P. and Allen, Michael J. and Clarke, Robert and Gera, Joseph and Hodgkinson, John (2005) Development and Testing of Control Laws for the Active Aeroelastic Wing Program. Technical Report NASA/TM-2005-213666, Research Engineering, NASA Dryden Flight Research Center.
Dibley, Ryan P. and Allen, Michael J. and Clarke, Robert and Gera, Joseph and Hodgkinson, John (2005) Development and Testing of Control Laws for the Active Aeroelastic Wing Program. Conference Paper AIAA-2005-6314, Research Engineering, NASA Dryden Flight Research Center.
Ray, R.J. and Hicks, J.W. and Alexander, R.I. (1988) Development of a Real-Time Aeroperformance Analysis Technique for the X-29A Advanced Technology Demonstrator. Technical Report NASA TM-100432, Research Engineering, NASA Dryden Flight Research Center.
Edwards, John W. and Deets, Dwain A. (1975) Development of a Remote Digital Augmentation System and Application to a Remotely Piloted Research Vehicle. Technical Report NASA Technical Note TN D-7941, Research Engineering, NASA Dryden Flight Research Center.
Gee, Shu W. and Carr, Peter C. and Winter, William R. and Manke, John A. (1978) Development of Systems and Techniques for Landing an Aircraft Using Onboard Television. Technical Report NASA TP-1171, Research Engineering, NASA Dryden Flight Research Center.
Johnson, J. Blair and Larson, Terry J. and Ficke, Jules M. (1987) Digital Program For Calculating Static Pressure Position Error. Technical Report NASA TM-86726, Research Engineering, NASA Dryden Flight Research Center.
España, Martin and Gilyard, Glenn (1995) Direct Adaptive Performance Optimization of Subsonic Transports: A Periodic Perturbation Technique. Technical Report NASA TM-4676, Research Engineering, NASA Dryden Flight Research Center.
Wilson, Ronald J. (1966) Drag and Wear Characteristics of Various Skid Materials on Dissimilar Lakebed Surfaces During the Slideout of the X-15 Airplane. Technical Report NASA Technical Note TN D-3331, Research Engineering, NASA Dryden Flight Research Center.
Montoya, Lawrence C. (1970) Drag Characteristics Obtained from Several Configurations of the Modified X-15-2 Airplane up to Mach 6.7. Technical Report NASA TM X-2056, Research Engineering, NASA Dryden Flight Research Center.
Corda, Stephen and Stephenson, Mark T. and Burcham Jr., Frank W. (1995) Dynamic Ground Effects Flight Test of an F-15 Aircraft. Electronic Workshop Presentation, Research Engineering, NASA Dryden Flight Research Center.
Gera, Joseph (1986) Dynamics and Controls Flight Testing of the X-29A Airplane. Technical Report NASA TM-86803, Research Engineering, NASA Dryden Flight Research Center.
Yuhas, Andrew J. and Ray, Ronald J. (1992) Effects of Bleed Air Extraction on Thrust Levels of the F404-GE-400 Turbofan Engine. Technical Report NASA TM-104247, Research Engineering, NASA Dryden Flight Research Center.
Kellogg, Gary V. and Wagner, Charles A. (1988) Effects of Update and Refresh Rates on Flight Simulation Visual Displays. Technical Report NASA TM-100415, Research Engineering, NASA Dryden Flight Research Center.
Drake, Hubert M. (1950) Effects on the Lateral Oscillation of Fixing the Rudder and Reflexing the Flaps on the Bell X-1 Airplane. Technical Report NACA RM L50I05, Research Engineering, NASA Dryden Flight Research Center.
Drake, Hubert M. and Clagett, Harry P. (1951) Effects on the Snaking Oscillation of the Bell X-1 Airplane of a Trailing-Edge Bulb on the Rudder. Technical Report NACA RM L50K01a, Research Engineering, NASA Dryden Flight Research Center.
Day, Richard E. (2004) Energy Management of Boost-Glide Vehicles: A Historical Perspective . Technical Report NASA/TP-2004-212037, Research Engineering, NASA Dryden Flight Research Center.
Ennix, Kimberly A. (1993) Engine Exhaust Characteristics Evaluation in Support of Acoustic Testing. Technical Report NASA TM-104263, Research Engineering, NASA Dryden Flight Research Center.
Bauer, Jeffrey E. and Andrisani, Dominick (1990) Estimating Short-Period Dynamics Using an Extended Kalman Filter. Technical Report NASA TM-101722, Research Engineering, NASA Dryden Flight Research Center.
Ray, Ronald J. (1994) Evaluating the Dynamic Response of In-Flight Thrust Calculation Techniques During Throttle Transients. Technical Report NASA TM-4591, Research Engineering, NASA Dryden Flight Research Center.
Larson, Terry J. (1984) Evaluation of a Flow Direction Probe and a Pitot-Static Probe on the F-14 Airplane at High Angles of Attack and Sideslip. Technical Report NASA TM-84911, Research Engineering, NASA Dryden Flight Research Center.
Lytton, Lee E. (1967) Evaluation of a Vertical-Scale, Fixed-Index Instrument Display Panel for the X-15 Airplane. Technical Report NASA Technical Note TN D-3967, Research Engineering, NASA Dryden Flight Research Center.
Jarvis, Calvin R. and Loschke, Paul C. and Enevoldson, Einar K. (1970) Evaluation of the Effect of a Yaw-Rate Damper on the Flying Qualities of a Light Twin-Engine Airplane. Technical Report NASA Technical Note TN D-5890, Research Engineering, NASA Dryden Flight Research Center.
Ray, Ronald J. (1990) Evaluation of Various Thrust Calibration Techniques on an F404 Engine. Technical Report NASA TP-3001, Research Engineering, NASA Dryden Flight Research Center.
Regenie, Victoria A. and Earls, Michael and Le, Jeanette and Thomson, Michael (1992) Experience With Ada on the F-18 High Alpha Research Vehicle Flight Test Program. Technical Report NASA TM-104259, Research Engineering, NASA Dryden Flight Research Center.
Fields, Roger A. and Olinger, Frank V. and Monaghan, Richard C. (1972) Experimental Investigation of Mach 3 Cruise Heating Simulations on a Representative Wing Structure For Flight-Loads Measurement. Technical Report NASA Technical Note TN D-6749, Research Engineering, NASA Dryden Flight Research Center.
Duke, Eugene L. and Regenie, Victoria A. (1985) Expert Systems Development and Application. Technical Report NASA TM-86746, Research Engineering, NASA Dryden Flight Research Center.
Iliff, Kenneth W. and Shafer, Mary F. (1993) Extraction of Stability and Control Derivatives From Other Flight Data. Technical Report NASA TM-4500, Research Engineering, NASA Dryden Flight Research Center.
Kehoe, Michael W. (1985) F-8 Refueling Boom Ground Vibration Test. Technical Report NASA TM-84914, Research Engineering, NASA Dryden Flight Research Center.
Vachon, M. Jake and Ray, Ronald J. and Walsh, Kevin R. and Ennix, Kimberly (2003) F/A-18 Performance Benefits Measured During the Autonomous Formation Flight Project. Technical Report NASA/TM-2003-210734, Research Engineering, NASA Dryden Flight Research Center.
Zavala, Eddie (1997) Fiber Optic Experience with the Smart Actuation System on the F-18 Systems Research Aircraft. Technical Report NASA/TM-97-206223, Research Engineering, NASA Dryden Flight Research Center.
Webb, Lannie D. and Andriyich-Varda, Dom and Whitmore, Stephen A. (1984) Flight and Wind-Tunnel Comparisons of the Inlet/Airframe Interaction of the F-15 Airplane. Technical Report NASA TP-2374, Research Engineering, NASA Dryden Flight Research Center.
Orme, John S. and Schkolnik, Gerard S. (1995) Flight Assessment of the Onboard Propulsion System Model for the Performance Seeking Control Algorithm on an F-15 Aircraft. Technical Report NASA TM-4705, Research Engineering, NASA Dryden Flight Research Center.
Sim, Alex G. (1984) Flight Characteristics of a Manned, Low-Speed, Controlled Deep Stall Vehicle. Technical Report NASA TM-86041, Research Engineering, NASA Dryden Flight Research Center.
Sitz, Joel R. and Vernon, Todd H. (1990) Flight Control System Design Factors for Applying Automated Testing Techniques. Technical Report NASA TM-4242, Research Engineering, NASA Dryden Flight Research Center.
Larson, Richard R. (1986) Flight Control System Development and Flight Test Experience with the F-111 Mission Adaptive Wing Aircraft. Technical Report NASA TM-88265, Research Engineering, NASA Dryden Flight Research Center.
Gilyard, Glenn B. and Smith, John W. and Falkner, Victor L. (1974) Flight Evaluation of a Mach 3 Cruise Longitudinal Autopilot. Meeting Paper AIAA-1974-910, Research Engineering, NASA Dryden Flight Research Center.
Curry, Robert E. and Gilyard, Glenn B. (1989) Flight Evaluation of a Pneumatic System for Unsteady Pressure Measurements Using Conventional Sensors. Technical Report NASA TM-4131, Research Engineering, NASA Dryden Flight Research Center.
Loschke, Paul C. and Barber, Marvin R. and Enevoldson, Einar K. and McMurtry, Thomas C. (1974) Flight Evaluation of Advanced Control Systems and Displays on a General Aviation Airplane. Technical Report NASA Technical Note TN D-7703, Research Engineering, NASA Dryden Flight Research Center.
Watts, Joe D. (1968) Flight Experience with Shock Impingement and Interference Heating on the X-15-2 Research Airplane. Technical Report NASA TM X-1669, Research Engineering, NASA Dryden Flight Research Center.
Putnam, Terrill W. (1974) Flight Experience with the Decelerating Noise Abatement Approach. Technical Report NASA TM X-56020, Research Engineering, NASA Dryden Flight Research Center.
Staff, NACA (1955) Flight Experience with Two High-Speed Airplanes Having Violent Lateral-Longitudinal Coupling in Aileron Rolls. Technical Report NACA RM H55A13, Research Engineering, NASA Dryden Flight Research Center.
Lock, Wilton P. and Kordes, Eldon E. and McKay, James M. and Wykes, John H. (1973) Flight Investigation of a Structural Mode Control System for the XB-70 Aircraft. Technical Report NASA Technical Note TN D-7420, Research Engineering, NASA Dryden Flight Research Center.
Perry, John J. and Dana, William H. and Bacon Jr., Donald C. (1967) Flight Investigation of the Landing Task in a Jet Trainer with Restricted Fields of View. Technical Report NASA Technical Note TN D-4018, Research Engineering, NASA Dryden Flight Research Center.
McKay, James M. and Kordes, Eldon E. and Wykes, John H. (1973) Flight Investigation of XB-70 Structural Response to Oscillatory Aerodynamic Shaker Excitation and Correlation with Analytical Results. Technical Report NASA Technical Note TN D-7227, Research Engineering, NASA Dryden Flight Research Center.
Lewis, Thomas L. and McLeod, Norman J. (1966) Flight Measurements of Boundary-Layer Noise on the X-15. Technical Report NASA Technical Note TN D-3364, Research Engineering, NASA Dryden Flight Research Center.
Pyle, Jon S. (1965) Flight Pressure Distributions on the Vertical Stabilizers and Speed Brakes of the X-15 Airplane at Mach Numbers from 1 to 6. Technical Report NASA Technical Note TN D-3048, Research Engineering, NASA Dryden Flight Research Center.
Putnam, Terrill W. and Ayers, Theodore G. (1988) Flight Research and Testing. Technical Report NASA TM-100439, Research Engineering, NASA Dryden Flight Research Center.
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Horton, Timothy W. and Kempel, Robert W. (1988) Flight Test Experience and Controlled Impact of a Remotely Piloted Jet Transport Aircraft. Technical Report NASA TM-4084, Research Engineering, NASA Dryden Flight Research Center.
Buschbacher, Mark and Maliska, Heather (2006) Flight Test of an Adaptive Controller and Simulated Failure/Damage on the NASA NF-15B. Meeting Presentation SFTE2006, Research Engineering, NASA Dryden Flight Research Center.
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Clarke, Robert and Allen, Michael J. and Dibley, Ryan P. and Gera, Joseph and Hodgkinson, John (2005) Flight Test of the F/A-18 Active Aeroelastic Wing Airplane. Meeting Paper AIAA-2005-6316, Research Engineering, NASA Dryden Flight Research Center.
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Hicks, John W. and Cooper Jr., James M. and Sefic, Walter J. (1987) Flight Test Techniques for the X-29A Aircraft. Technical Report NASA TM-88289, Research Engineering, NASA Dryden Flight Research Center.
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Ward, Donald T. and Dorsett, Kenneth M. (1993) Flight Validation of a Pulsed Smoke Flow Visualization System. Technical Report NASA CR-186026, Research Engineering, NASA Dryden Flight Research Center.
Fields, Roger A. (1992) Flight Vehicle Thermal Testing With Infrared Lamps. Technical Report NASA TM-4336, Research Engineering, NASA Dryden Flight Research Center.
Marshall, Robert T. (1971) Flight-Determined Acceleration and Climb Performance of an F-104G Airplane for Use in an Optimum-Flight-Path Computer Program. Technical Report NASA Technical Note TN D-6398, Research Engineering, NASA Dryden Flight Research Center.
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Hughes, Donald L. and Holzman, Jon K. and Johnson, Harold J. (1972) Flight-Determined Characteristics of an Air Intake System on an F-111A Airplane. Technical Report NASA Technical Note TN D-6679, Research Engineering, NASA Dryden Flight Research Center.
Ennix, Kimberly A. and Burcham Jr., Frank W. and Webb, Lannie D. (1993) Flight-Determined Engine Exhaust Characteristics of an F404 Engine in an F-18 Airplane. Technical Report NASA TM-4538, Research Engineering, NASA Dryden Flight Research Center.
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Arnaiz, Henry H. (1977) Flight-Measured Lift and Drag Characteristics of a Large, Flexible, High Supersonic Cruise Airplane. Technical Report NASA TM X-3532, Research Engineering, NASA Dryden Flight Research Center.
Tang, Ming H. and Pearson, George P. E. (1973) Flight-Measured X-24A Lifting Body Control-Surface Hinge Moments and Correlation with Wind-Tunnel Predictions. Technical Report NASA TM X-2816, Research Engineering, NASA Dryden Flight Research Center.
Reukauf, Paul J. and Schweikhard, William G. and Arnaiz, Henry (1974) Flight-Test Techniques for Obtaining Valid Comparisons of Wind-Tunnel and Flight Results from Tests on a YF-12 Mixed-Compression Inlet. Meeting Paper AIAA-1974-1195, Research Engineering, NASA Dryden Flight Research Center.
Davis, Mark C. and White, J. Terry (2006) Flight-Test-Determined Aerodynamic Force and Moment Characteristics of the X-43A at Mach 7.0. Meeting Presentation AIAA-2006-8028, Research Engineering, NASA Dryden Flight Research Center.
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Freudinger, Lawrence C. (1989) Flutter Clearance of the F-18 High-Angle-of-Attack Research Vehicle With Experimental Wingtip Instrumentation Pods. Technical Report NASA TM-4148, Research Engineering, NASA Dryden Flight Research Center.
Kehoe, Michael W. and Ellison, Joseph F. (1985) Flutter Clearance of the Schweizer 1-36 Deep-Stall Sailplane. Technical Report NASA TM-85917, Research Engineering, NASA Dryden Flight Research Center.
Lind, Rick and Brenner, Marty (2000) Flutterometer: An On-Line Tool to Predict Robust Flutter Margins. Journal of Aircraft 37(6):1105-1112.
Whitmore, Stephen A. (1985) Formulation and Implementation of Nonstationary Adaptive Estimation Algorithm With Applications to Air-Data Reconstruction. Technical Report NASA TM-86727, Research Engineering, NASA Dryden Flight Research Center.
Whitmore, Stephen A. (1988) Formulation of a General Technique for Predicting Pneumatic Attenuation Errors in Airborne Pressure Sensing Devices. Technical Report NASA TM-100430, Research Engineering, NASA Dryden Flight Research Center.
Sefic, Walter J. (1979) Friction Characteristics of Steel Skids Equipped with Skegs on a Lakebed Surface. Technical Report NASA TM-81347, Research Engineering, NASA Dryden Flight Research Center.
Conners, Timothy R. and Sims, Robert L. (1998) Full Flight Envelope Direct Thrust Measurement on a Supersonic Aircraft. Technical Report NASA/TM-1998-206560, Research Engineering, NASA Dryden Flight Research Center.
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Murray, James E. and Pahle, Joseph W. and Thornton, Stephen V. and Vogus, Shannon and Frackowiak, Tony and Mello, Joe and Norton, Brook (2002) Ground and Flight Evaluation of a Small-Scale Inflatable-Winged Aircraft. Technical Report NASA/TM-2002-210721, Research Engineering, NASA Dryden Flight Research Center.
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Voracek, David F. (1993) Ground Vibration and Flight Flutter Tests of the Single-Seat F-16XL Aircraft With a Modified Wing. Technical Report NASA TM-104264, Research Engineering, NASA Dryden Flight Research Center.
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Kehoe, Michael W. and Voracek, David F. (1989) Ground Vibration Test Results of a JetStar Airplane Using Impulsive Sine Excitation. Technical Report NASA TM-100448, Research Engineering, NASA Dryden Flight Research Center.
Cobleigh, Brent R. (1994) High-Angle-of-Attack Yawing Moment Asymmetry of the X-31 Aircraft from Flight Test. Technical Report NASA CR-186030, Research Engineering, NASA Dryden Flight Research Center.
Hewett, Marle D. (1992) High-Speed Civil Transport Issues and Technology Program. Technical Report NASA CR-186020, Research Engineering, NASA Dryden Flight Research Center.
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Bellman, Donald R. and Kier, David A. (1974) HiMAT – A New Approach to the Design of Highly Maneuverable Aircraft. Meeting Paper SAE Paper 740859, Research Engineering, NASA Dryden Flight Research Center.
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Schkolnik, Gerard S. (1993) Identification of Integrated Airframe–Propulsion Effects on an F-15 Aircraft for Application to Drag Minimization. Technical Report NASA TM-4532, Research Engineering, NASA Dryden Flight Research Center.
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Vernon, Lura (1993) In-flight Investigation of a Rotating Cylinder-Based Structural Excitation System for Flutter Testing. Technical Report NASA TM-4512, Research Engineering, NASA Dryden Flight Research Center.
Richwine, David M. and Fisher, David F. (1992) In-Flight Leading Edge Extension Vortex Flow-Field Survey Measurements on a F-18 Aircraft at High Angle of Attack. Technical Report NASA TM-4398, Research Engineering, NASA Dryden Flight Research Center.
Saltzman, Edwin J. and Hicks, John W. (1994) In-Flight Lift-Drag Characteristics for a Forward-Swept-Wing Aircraft (and Comparisons With Contemporary Aircraft). Technical Report NASA TP-3414, Research Engineering, NASA Dryden Flight Research Center.
Trujillo, Bianca M. and Meyer Jr., Robert R. and Sawko, Paul M. (1983) In-Flight Load Testing of Advanced Shuttle Thermal Protection Systems. Technical Report NASA TM-86024, Research Engineering, NASA Dryden Flight Research Center.
Shafer, Mary F. (1992) In-Flight Simulation Studies at the NASA Dryden Flight Research Facility. Technical Report NASA TM-4396, Research Engineering, NASA Dryden Flight Research Center.
Corda, Stephen and Franz, Russell J. and Blanton, James N. and Vachon, M. Jake and DeBoer, James B. (2002) In-Flight Vibration Environment of the NASA F-15B Flight Test Fixture. Technical Report NASA/TM-2002-210719, Research Engineering, NASA Dryden Flight Research Center.
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Carpenter, Richard and Thompson, Milton O. and Bowers, Joseph H. (1971) Instrumentation and Drop-Testing Techniques for Investigating Flight Vehicles and Personnel Protective Systems. Technical Report NASA TM X-2149, Research Engineering, NASA Dryden Flight Research Center.
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Fulton Jr., Fitzhugh L. (1968) Lessons from the XB-70 as Applied to the Supersonic Transport. Technical Report NASA TM X-56014, Research Engineering, NASA Dryden Flight Research Center.
Pyle, Jon S. and Swanson, Robert H. (1967) Lift and Drag Characteristics of the M2-F2 Lifting Body During Subsonic Gliding Flight. Technical Report NASA TM X-1431, Research Engineering, NASA Dryden Flight Research Center.
Nugent, Jack (1956) Lift and Drag of the Bell X-5 Research Airplane in the 45 Degree Sweptback Configuration at Transonic Speeds. Technical Report NACA RM H56E02, Research Engineering, NASA Dryden Flight Research Center.
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Putnam, Terrill W. and Lasagna, Paul L. and White, Kenneth C. (1975) Measurements and Analysis of Aircraft Airframe Noise. Conference Paper AIAA-1975-510, Research Engineering, NASA Dryden Flight Research Center.
Drake, Hubert M. (1949) Measurements of Aileron Effectiveness of the Bell X-1 Airplane at Mach Numbers Between 0.9 and 1.06. Technical Report NACA RM L9G19a, Research Engineering, NASA Dryden Flight Research Center.
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Lewis, Thomas L. and Dods Jr., Jules B. and Hanly, Richard D. (1973) Measurements of Surface-Pressure Fluctuations on the XB-70 Airplane at Local Mach Numbers up to 2.45. Technical Report NASA Technical Note TN D-7226, Research Engineering, NASA Dryden Flight Research Center.
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Nissim, E. and Gilyard, Glenn B. (1989) Method for Experimental Determination of Flutter Speed by Parameter Identification. Technical Report NASA TP-2923, Research Engineering, NASA Dryden Flight Research Center.
Orme, John S. and Nobbs, Steven G. (1995) Minimum Fan Turbine Inlet Temperature Mode Evaluation. Electronic Workshop Presentation, Research Engineering, NASA Dryden Flight Research Center.
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Kehoe, Michael W. (1986) Modified U.S. Army U-8F Ground Vibration Test. Technical Report NASA TM-86741, Research Engineering, NASA Dryden Flight Research Center.
Voracek, David F. (1990) Monitoring Techniques for the X-29A Aircraft's High-Speed Rotating Power Takeoff Shaft. Technical Report NASA TM-101731, Research Engineering, NASA Dryden Flight Research Center.
Layton, Garrison P. (1974) NASA Flight Research Center Scale F-15 Remotely Piloted Research Vehicle Program. Meeting Paper SFTE 05-02, Research Engineering, NASA Dryden Flight Research Center.
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España, Martin D. and Gilyard, Glenn B. (1993) On the Estimation Algorithm Used in Adaptive Performance Optimization of Turbofan Engines. Technical Report NASA TM-4551, Research Engineering, NASA Dryden Flight Research Center.
Gilyard, Glenn and España, Martin (1994) On the Use of Controls for Subsonic Transport Performance Improvement: Overview and Future Directions. Technical Report NASA TM-4605, Research Engineering, NASA Dryden Flight Research Center.
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Budd, Gerald D. and Gilman, Ronald L. and Eichstedt, David (1993) Operational and Research Aspects of a Radio-Controlled Model Flight Test Program. Meeting Paper AIAA-1993-0625, Research Engineering, NASA Dryden Flight Research Center.
Deets, Dwain A. and Purifoy, Dana (1998) Operational Concepts for Uninhabited Tactical Aircraft. Technical Report NASA/TM-1998-206549, Research Engineering, NASA Dryden Flight Research Center.
Jarvis, Calvin R. and Lock, Wilton P. (1965) Operational Experience with the X-15 Reaction Control and Reaction Augmentation Systems. Technical Report NASA Technical Note TN D-2864, Research Engineering, NASA Dryden Flight Research Center.
Chacon, Vince and McBride, David (1988) Operational Viewpoint of the X-29A Digital Flight Control System. Technical Report NASA TM-100434, Research Engineering, NASA Dryden Flight Research Center.
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Meyer, Robert R. (1992) Overview of the NASA Dryden Flight Research Facility Aeronautical Flight Projects. Technical Report NASA TM-104254, Research Engineering, NASA Dryden Flight Research Center.
Pyle, Jon S. and Phelps, James R. and Baron, Robert S. (1973) Performance of a Ballute Decelerator Towed Behind a Jet Airplane. Technical Report NASA TM X-56019, Research Engineering, NASA Dryden Flight Research Center.
Navarro, Robert (1997) Performance of an Electro-Hydrostatic Actuator on the F-18 Systems Research Aircraft. Technical Report NASA/TM-97-206224, Research Engineering, NASA Dryden Flight Research Center.
Schkolnik, Gerard (1995) Performance Seeking Control Excitation Mode. Electronic Workshop Presentation, Research Engineering, NASA Dryden Flight Research Center.
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Murray, James and Moes, Timothy and Norlin, Ken and Bauer, Jeffrey and Geenen, Robert and Moulton, Bryan and Hoang, Stephen (1992) Piloted Simulation Study of a Balloon-Assisted Deployment of an Aircraft at High Altitude. Technical Report NASA TM-104245, Research Engineering, NASA Dryden Flight Research Center.
Conners, Timothy R. (1997) Predicted Performance of a Thrust-Enhanced SR-71 Aircraft with an External Payload. Technical Report NASA TM-104330, Research Engineering, NASA Dryden Flight Research Center.
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Haering Jr., Edward A. and Ehernberger, L. J. and Whitmore, Stephen A. (1995) Preliminary Airborne Measurements for the SR-71 Sonic Boom Propagation Experiment. Technical Report NASA TM-104307, Research Engineering, NASA Dryden Flight Research Center.
Ward, Donald T. and Myatt, James H. (1993) Preliminary Design of an Intermittent Smoke Flow Visualization System. Technical Report NASA CR-186027, Research Engineering, NASA Dryden Flight Research Center.
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Hicks, John W. and Matheny, Neil W. (1987) Preliminary Flight Assessment of the X-29A Advanced Technology Demonstrator. Technical Report NASA TM-100407, Research Engineering, NASA Dryden Flight Research Center.
Wolowicz, Chester H. and Strutz, Larry W. and Gilyard, Glenn B. and Matheny, Neil W. (1968) Preliminary Flight Evaluation of the Stability and Control Derivatives and Dynamic Characteristics of the Unaugmented XB-70-1 Airplane Including Comparisons With Predictions. Technical Report NASA Technical Note TN D-4578, Research Engineering, NASA Dryden Flight Research Center.
Burcham, Frank W. and Maine, Trindel A. and Fullerton, C. Gordon and Wells, Edward A. (1993) Preliminary Flight Results of a Fly-by-Throttle Emergency Flight Control System on an F-15 Airplane. Technical Report NASA TM-4503, Research Engineering, NASA Dryden Flight Research Center.
Hicks, John W. and Huckabone, Thomas (1989) Preliminary Flight-Determined Subsonic Lift and Drag Characteristics of the X-29A Forward-Swept-Wing Airplane. Technical Report NASA TM-100409, Research Engineering, NASA Dryden Flight Research Center.
Lasagna, Paul L. and McLeod, Norman J. (1968) Preliminary Measured and Predicted XB-70 Engine Noise. Technical Report NASA TM X-1565, Research Engineering, NASA Dryden Flight Research Center.
Lasagna, Paul L. and Putnam, Terrill W. (1974) Preliminary Measurements of Aircraft Aerodynamic Noise. Meeting Paper AIAA-1974-572, Research Engineering, NASA Dryden Flight Research Center.
Kordes, Eldon E. and Tanner, Carole S. (1964) Preliminary Results of Boundary-Layer Noise Measured on the X-15 Airplane. Technical Report NASA TM X-56003, Research Engineering, NASA Dryden Flight Research Center.
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Hodge, Kenneth E. (Compiled by) (1996) Proceedings of the F-8 Digital Fly-By-Wire and Supercritical Wing First Flight's 20th Anniversary Celebration, Volume II. Technical Report NASA Conference Publication CP-3256, Volume II, Research Engineering, NASA Dryden Flight Research Center.
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Larson, Terry J. and Whitmore, Stephen A. and Ehernberger, L. J. and Johnson, J. Blair and Siemers III, Paul M. (1987) Qualitative Evaluation of a Flush Air Data System at Transonic Speeds and High Angles of Attack. Technical Report NASA TP-2716, Research Engineering, NASA Dryden Flight Research Center.
Spivey, Natalie D. and Herrera, Claudia Y. and Truax, Roger and Pak, Chan-gi and Freund, Donald (2007) Quiet Spike™ Build-up Ground Vibration Testing Approach. Technical Report NASA/TM-2007-214625, Research and Engineering, NASA Dryden Flight Research Center.
Spivey, Natalie D. and Herrera, Claudia Y. and Truax, Roger and Pak, Chan-gi and Freund, Donald (2007) Quiet Spike™ Build-up Ground Vibration Testing Approach. Conference Presentation AIAA-2007-1775, Research and Engineering, NASA Dryden Flight Research Center.
Conners, Timothy R. and Nobbs, Steven G. and Orme, John S. (1995) Rapid Deceleration Mode Evaluation. Electronic Workshop Presentation, Research Engineering, NASA Dryden Flight Research Center.
Mackall, Dale and Norlin, Kenneth and Cohen, Dorothea and Kellogg, Gary and Schilling, Lawrence and Sheen, John (1992) Rapid Development of the X-31 Simulation to Support Flight-Testing. Technical Report NASA TM-104256, Research Engineering, NASA Dryden Flight Research Center.
Hicks, John W. and Petersen, Kevin L. (1988) Real-Time Flight Test Analysis and Display Techniques for the X-29A Aircraft. Technical Report NASA TM-101692, Research Engineering, NASA Dryden Flight Research Center.
Ray, Ronald J. and Hicks, John W. and Wichman, Keith D. (1991) Real-Time In-Flight Engine Performance and Health Monitoring Techniques for Flight Research Application. Technical Report NASA TM-104239, Research Engineering, NASA Dryden Flight Research Center.
Del Frate, John H. and Cosentino, Gary B. (1998) Recent Flight Test Experience with Uninhabited Aerial Vehicles at the NASA Dryden Flight Research Center. Technical Report NASA/TM-1998-206546, Research Engineering, NASA Dryden Flight Research Center.
Tymczyszyn, Joseph J. and Barber, Marvin R. (1974) Recent Wake Turbulence Flight Test Programs. Conference Paper SETP Paper No. 1466, Research Engineering, NASA Dryden Flight Research Center.
Budd, Gerald D. and Gilman, Ronald L. and Eichstedt, David (1993) Research Aspects of a Radio-Controlled Model Flight Test Program. Technical Report NASA TM-104266, Research Engineering, NASA Dryden Flight Research Center.
Wilson, Ronald J. and Cazier Jr., Frank W. and Larson, Richard R. (1973) Results of Ground Vibration Tests on a YF-12 Airplane. Technical Report NASA TM X-2880, Research Engineering, NASA Dryden Flight Research Center.
Lind, Rick and Brenner, Marty (1997) Robust Flutter Margins of an F/A-18 Aircraft from Aeroelastic Flight Data. Journal of Guidance, Control, and Dynamics 20(3):597-604.
Szalai, Kenneth J. (1984) Role of Research Aircraft in Technology Development. Technical Report NASA TM-85913, Research Engineering, NASA Dryden Flight Research Center.
Painter, W. D. and Erickson, R. E. (1984) Rotor Systems Research Aircraft Airplane Configuration Flight-Test Results. Technical Report NASA TM-85911, Research Engineering, NASA Dryden Flight Research Center.
Orme, John S. and Sims, Robert L. (1999) Selected Performance Measurements of the F-15 ACTIVE Axisymmetric Thrust-Vectoring Nozzle. Meeting Paper ISABE Paper IS-166, Research Engineering, NASA Dryden Flight Research Center.
Lokos, William A. and Lizotte, Andrew and Lindsley, Ned J. and Stauf, Rick (2005) Shock Location Dominated Transonic Flight Loads on the Active Aeroelastic Wing. Technical Report NASA/TM-2005-213667, Research Engineering, NASA Dryden Flight Research Center.
Lokos, William A. and Lizotte, Andrew and Lindsley, Ned J. and Stauf, Rick (2005) Shock Location Dominated Transonic Flight Loads on the Active Aeroelastic Wing. Conference Presentation AIAA-2005-6315, Research Engineering, NASA Dryden Flight Research Center.
Wolowicz, Chester H. and Bowman Jr., James S. and Gilbert, William P. (1979) Similitude Requirements and Scaling Relationships as Applied to Model Testing. Technical Report NASA Technical Paper TP-1435, Research Engineering, NASA Dryden Flight Research Center.
Smith, John P. and Schilling, Lawrence J. and Wagner, Charles A. (1989) Simulation at Dryden Flight Research Facility From 1957 to 1982. Technical Report NASA TM-101695, Research Engineering, NASA Dryden Flight Research Center.
Hudson, Larry D. and Thompson, Randolph C. (1991) Single-Strain-Gage Force/Stiffness Buckling Prediction Techniques On A Hat-Stiffened Panel. Technical Report NASA TM-101733, Research Engineering, NASA Dryden Flight Research Center.
Fisher, David F. (2007) Six Decades of Flight Research: An Annotated Bibliography of Technical Publications of NASA Dryden Flight Research Center, 1946-2006. Technical Report NASA/TP-2007-213684, Research Engineering, NASA Dryden Flight Research Center.
Petersen, Kevin L. and Flores Jr., Christobal (1984) Software Control and System Configuration Management: A Systems-Wide Approach. Technical Report NASA TM-85908, Research Engineering, NASA Dryden Flight Research Center.
Iliff, Kenneth W. and Shafer, Mary F. (1993) Space Shuttle Hypersonic Aerodynamic and Aerothermodynamic Flight Research and the Comparison to Ground Test Results. Technical Report NASA TM-4499, Research Engineering, NASA Dryden Flight Research Center.
Moua, Cheng M. and Cox, Timothy H. and McWherter, Shaun C. (2008) Stability and Controls Analysis and Flight Test Results of a 24-Foot Telescoping Nose Boom on an F-15B Airplane. Meeting Presentation AIAA-2008-0126, Research and Engineering, NASA Dryden Flight Research Center.
Wilson, Ronald J. (1967) Statistical Analysis of Landing Contact Conditions of the X-15 Airplane. Technical Report NASA Technical Note TN D-3801, Research Engineering, NASA Dryden Flight Research Center.
Wilson, Ronald J. and Larson, Richard R. (1967) Statistical Analysis of Landing-Contact Conditions for the XB-70 Airplane. Technical Report NASA Technical Note TN D-4007, Research Engineering, NASA Dryden Flight Research Center.
Lokos, William A. and Olney, Candida D. and Chen, Tony and Crawford, Natalie D. and Stauf, Rick and Reichenbach, Eric (2002) Strain Gage Loads Calibration Testing of the Acitve Aeroelastic Wing F/A-18 Aircraft. Technical Report NASA/TM-2002-210726, Research Engineering, NASA Dryden Flight Research Center.
Lokos, William A. and Stauf, Rick (2004) Strain-Gage Loads Calibration Parametric Study. Technical Report NASA/TM-2004-212853, Research Engineering, NASA Dryden Flight Research Center.
Nelson II, Sigurd A. (1994) Strain-Gage Selection in Loads Equations Using a Genetic Algorithm. Technical Report NASA CR-4597, Research Engineering, NASA Dryden Flight Research Center.
Gilyard, Glenn B. and Orme, John S. (1992) Subsonic Flight Test Evaluation of a Performance Seeking Control Algorithm on an F-15 Airplane. Technical Report NASA TM-4400, Research Engineering, NASA Dryden Flight Research Center.
Orme, John S. and Gilyard, Glenn B. (1992) Subsonic Flight Test Evaluation of a Propulsion System Parameter Estimation Process for the F100 Engine. Technical Report NASA TM-4426, Research Engineering, NASA Dryden Flight Research Center.
Orme, John S. (1995) Summary of Performance Seeking Control (PSC) for the
F-15 Highly Integrated Digital Electronic Control (HIDEC) Aircraft. Electronic Workshop Presentation, Research Engineering, NASA Dryden Flight Research Center.
Andrews, William H. (1966) Summary of Preliminary Data Derived from the XB-70 Airplanes. Technical Report NASA TM X-1240, Research Engineering, NASA Dryden Flight Research Center.
Walsh, Kevin R. (1993) Summary of the Effects of Engine Throttle Response on Airplane Formation-Flying Qualities. Technical Report NASA TM-4465, Research Engineering, NASA Dryden Flight Research Center.
Guckenberger, Dutch and Uliano, Kevin C. and Lane, Norman E. (1993) Teaching High-Performance Skills Using Above-Real-Time Training. Technical Report NASA CR-4528, Research Engineering, NASA Dryden Flight Research Center.
Arnaiz, Henry H. (1975) Techniques for Determining Propulsion System Forces for Accurate High Speed Vehicle Drag Measurements in Flight. Conference Paper AIAA-1975-964, Research Engineering, NASA Dryden Flight Research Center.
DeAngelis, V. Michael and Fields, Roger A. (1990) Techniques for Hot Structures Testing. Technical Report NASA TM-101727, Research Engineering, NASA Dryden Flight Research Center.
Voracek, David and Pendleton, Ed and Griffin, Dr. Kenneth and Reichenbach, Eric and Welch, Leslie (2003) The Active Aeroelastic Wing Phase I Flight Research Through January 2003. Technical Report NASA/TM-2003-210741, Research Engineering, NASA Dryden Flight Research Center.
Jenkins, Jerald M. (1980) The Effect of Thermal Stresses on the Integrity of Three Built-Up Aircraft Structures. Technical Report NASA TM-81352, Research Engineering, NASA Dryden Flight Research Center.
Nissim, E. (1990) The Effectiveness of Vane-Aileron Excitation in the Experimental Determination of Flutter Speed by Parameter Identification. Technical Report NASA TP-2971, Research Engineering, NASA Dryden Flight Research Center.
Voracek, David F. and Morales, Adolfo M. (1988) The Effects of Excitation Waveforms and Shaker Moving Mass on the Measured Modal Characteristics of a 2- by 5-Foot Aluminum Plate. Technical Report NASA TM-100446, Research Engineering, NASA Dryden Flight Research Center.
Regenie, Victoria and Gatlin, Donald and Kempel, Robert and Matheny, Neil (1992) The F-18 High Alpha Research Vehicle: A High-Angle-of-Attack Testbed Aircraft. Technical Report NASA TM-104253, Research Engineering, NASA Dryden Flight Research Center.
Redifer, Matthew and Lin, Yohan and Bessent, Courtney Amos and Barklow, Carole (2007) The Hyper-X Flight Systems Validation Program. Technical Report NASA/TM-2007-214620, Research Engineering, NASA Dryden Flight Research Center.
Szalai, Kenneth J. (1967) The Influence of Response Feedback Loops on the Lateral-Directional Dynamics of a Variable-Stability Transport Aircraft. Technical Report NASA Technical Note TN D-3966, Research Engineering, NASA Dryden Flight Research Center.
Shy, Karla S. and Hageman, Jacob J. and Le, Jeanette H. (2002) The Role of Aircraft Simulation in Improving Flight Safety Through Control Training. Technical Report NASA/TM-2002-210731, Research Engineering, NASA Dryden Flight Research Center.
Evans, Martha B. and Schilling, Lawrence J. (1984) The Role of Simulation in the Development and Flight Test of the HiMAT Vehicle. Technical Report NASA TM-84912, Research Engineering, NASA Dryden Flight Research Center.
Cohen, Dorothea and Le, Jeanette H. (1991) The Role of the Remotely Augmented Vehicle (RAV) Laboratory in Flight Research. Technical Report NASA TM-104235, Research Engineering, NASA Dryden Flight Research Center.
Corda, Stephen and Moes, Timothy R. and Mizukami, Masashi and Hass, Neal E. and Jones, Daniel and Monaghan, Richard C. and Ray, Ronald J. and Jarvis, Michele L. and Palumbo, Nathan (2000) The SR-71 Test Bed Aircraft: A Facility for High-Speed Flight Research. Technical Report NASA/TP-2000-209023, Research Engineering, NASA Dryden Flight Research Center.
Sanderson, Kenneth C. (1964) The X-15 Flight Test Instrumentation. Technical Report NASA TM X-56000, Research Engineering, NASA Dryden Flight Research Center.
Bosworth, John T. and Stoliker, P. C. (1996) The X-31A Quasi-Tailless Flight Test Results. Technical Report NASA TP-3624, Research Engineering, NASA Dryden Flight Research Center.
Baumann, Ethan and Bahm, Catherine and Strovers, Brian and Beck, Roger and Richard, Michael (2007) The X-43A Six Degree of Freedom Monte Carlo Analysis. Technical Report NASA/TM-2007-214630, Research and Engineering, NASA Dryden Flight Research Center.
Baumann, Ethan and Bahm, Catherine and Strovers, Brian and Beck, Roger and Richard, Michael (2008) The X-43A Six Degree of Freedom Monte Carlo Analysis. Meeting Presentation AIAA-2008-0203, Research and Engineering, NASA Dryden Flight Research Center.
DeAngelis, V. Michael and Anderson, Karl F. (1992) Thermal-Structural Test Facilities at NASA Dryden. Technical Report NASA TM-104249, Research Engineering, NASA Dryden Flight Research Center.
Kehoe, Michael W. and Snyder, H. Todd (1991) Thermoelastic Vibration Test Techniques. Technical Report NASA TM-101742, Research Engineering, NASA Dryden Flight Research Center.
Saltzman, Edwin J. and Asher, William P. (1957) Transonic Flight Evaluation of the Effects of Fuselage Extension and Indentation on the Drag of a 60 Degree Delta-Wing Interceptor Airplane. Technical Report NACA RM H57E29, Research Engineering, NASA Dryden Flight Research Center.
Zuniga, Fanny A. and Drake, Aaron and Kennelly Jr., Robert A. and Koga, Dennis J. and Westphal, Russell V. (1994) Transonic Flight Test of a Laminar Flow Leading Edge With Surface Excrescences. Technical Report NASA TM-4597, Research Engineering, NASA Dryden Flight Research Center.
Lizotte, Andrew M. and Allen, Michael J. (2005) Twist Model Development and Results From the Active Aeroelastic Wing F/A-18 Aircraft. Technical Report NASA/TM-2005-212861, Research Engineering, NASA Dryden Flight Research Center.
Lizotte, Andrew M. and Allen, Michael J. (2007) Twist Model Development and Results from the Active Aeroelastic Wing F/A-18 Aircraft. Meeting Paper IF-078, Research Engineering, NASA Dryden Flight Research Center.
Rezek, Terrence W. (1983) Unmanned Vehicle System Experiences at the Dryden Flight Research Facility. Technical Report NASA TM-84913, Research Engineering, NASA Dryden Flight Research Center.
Chacon, Vince and Pahle, Joseph W. and Regenie, Victoria A. (1990) Validation of the F-18 High Alpha Research Vehicle Flight Control and Avionics Systems Modifications. Technical Report NASA TM-101723, Research Engineering, NASA Dryden Flight Research Center.
Larson, Terry J. and Schweikhard, William G. (1971) Verification of Takeoff Performance Predictions for the XB-70 Airplane. Technical Report NASA TM X-2215, Research Engineering, NASA Dryden Flight Research Center.
Tang, Ming H. (1971) Vertical-Fin Loads and Rudder Hinge-Moment Measurements on a 1/8-Scale Model of the M2-F3 Lifting Body Vehicle at Mach Numbers from 0.50 to 1.30. Technical Report NASA TM X-2286, Research Engineering, NASA Dryden Flight Research Center.
Lind, Rick and Brenner, Marty and Freudinger, Lawrence C. (1999) Wavelet Applications for Flight Flutter Testing. Conference Presentation NASA/CP-1999-209136/PT 1 Paper No. 33, Research Engineering, NASA Dryden Flight Research Center.
Montoya, Earl J. and Palitz, Murray (1967) Wind-Tunnel Investigation of the Flow Field Beneath the Fuselage of the X-15 Airplane at Mach Numbers from 4 to 8. Technical Report NASA TM X-1469, Research Engineering, NASA Dryden Flight Research Center.
Whitmore, Stephen A. and Sprague, Stephanie and Naughton, Jonathan W. (2001) Wind-Tunnel Investigations of Blunt-Body Drag Reduction Using Forebody Surface Roughness. Technical Report NASA/TM-2001-210390, Research Engineering, NASA Dryden Flight Research Center.
Whitmore, Stephen A. and Sprague, Stephanie and Naughton, Jonathan W. (2001) Wind-Tunnel Investigations of Blunt-Body Drag Reduction Using Forebody Surface Roughness. Meeting Paper AIAA-2001-252, Research Engineering, NASA Dryden Flight Research Center.
Lokos, William A. and Olney, Candida D. and Crawford, Natalie D. and Stauf, Rick and Reichenbach, Eric Y. (2002) Wing Torsional Stiffness Tests of the Active Aeroelastic Wing F/A-18 Airplane. Technical Report NASA/TM-2002-210723, Research Engineering, NASA Dryden Flight Research Center.
Clarke, Robert and Burken, John J. and Bosworth, John T. and Bauer, Jeffrey E. (1994) X-29 Flight Control System: Lessons Learned. Technical Report NASA TM-4598, Research Engineering, NASA Dryden Flight Research Center.
Putnam, Terrill W. (1984) X-29 Flight-Research Program. Technical Report NASA TM-86025, Research Engineering, NASA Dryden Flight Research Center.
Sims, Robert and McCrosson, Paul and Ryan, Robert and Rivera, Joe (1989) X-29A Aircraft Structural Loads Flight Testing. Technical Report NASA TM-101715, Research Engineering, NASA Dryden Flight Research Center.
Trippensee, Gary A. and Lux, David P. (1987) X-29A Forward-Swept-Wing Flight Research Program Status. Technical Report NASA TM-100413, Research Engineering, NASA Dryden Flight Research Center.
Bowers, Albion H. (1984) X-29A Longitudinal and Directional Force and Moment Supplemental Transonic Wind Tunnel Test Results. Technical Report NASA TM-85909, Research Engineering, NASA Dryden Flight Research Center.
Sefic, Walter J. and Maxwell, Cleo M. (1986) X-29A Technology Demonstrator Flight Test Program Overview. Technical Report NASA TM-86809, Research Engineering, NASA Dryden Flight Research Center.
Vachon, Michael Jacob and Grindle, Thomas J. and St. John, Clinton W. and Dowdell, David B. (2005) X-43A Fluid and Environmental Systems: Ground and Flight Operation and Lessons Learned. Conference Presentation AIAA-2005-3337, Research Engineering, NASA Dryden Flight Research Center.
This list was generated on Fri Oct 10 18:15:22 PDT 2008.
