Subject: F-15
Number of records: 112.
McRae, D.S. and Peake, D.J. and Fisher, D.F. (1980) A Computational and Experimental Study of High Reynolds Number Viscous/Inviscid Interaction About a Cone at High Angle of Attack. Meeting Paper AIAA-1980-1422, Research Engineering, NASA Dryden Flight Research Center.
Layton, Garrison P. (1976) A New Experimental Flight Research Technique: The Remotely Piloted Airplane. Conference Paper AGARD-CP-187, Research Engineering, NASA Dryden Flight Research Center.
Maine, Trindel A. and Gilyard, Glenn B. and Lambert, Heather H. (1990) A Preliminary Evaluation of an F100 Engine Parameter Estimation Process Using Flight Data. Technical Report NASA TM-4216, 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. Meeting Paper AIAA-1991-2222, Research Engineering, NASA Dryden Flight Research Center.
Deets, Dwain A. and Edwards, John W. (1974) A Remotely Augmented Vehicle Approach to Flight Testing RPV Control Systems. Technical Report NASA TM X-56029, Reseach Engineering, NASA Dryden Flight Research Center.
Lambert, Heather H. (1991) A Simulation Study of Turbofan Engine Deterioration Estimation Using Kalman Filtering Techniques. Technical Report NASA TM-104233, Research Engineering, NASA Dryden Flight Research Center.
Ishmael, Stephen D. and McMonagle, Donald R. (1983) AFTI/F-16 Flight Test Results and Lessons. Technical Report NASA TM-84920, 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.
Zeis Jr., Capt Joseph E. and Lambert, Heather H. and Calico, Robert A. and Gleason, Maj Daniel (1988) Angle of Attack Estimation Using an Inertial Reference Platform. Meeting Paper AIAA-1988-4351, Research Engineering, NASA Dryden Flight Research Center.
Antoniewicz, Robert F. and Duke, Eugene L. and Menon, P. K. A. (1991) Application and Flight Test of Linearizing Transformations Using Measurement Feedback to the Nonlinear Control Problem. Technical Report NASA TP-3154, Research Engineering, NASA Dryden Flight Research Center.
Walton, James T. and Burcham Jr., Frank W. (1986) Augmentor Performance of an F100 Engine Model Derivative Engine in an F-15 Airplane. Technical Report NASA TM-86745, Research Engineering, NASA Dryden Flight Research Center.
Bohn-Meyer, Marta R. (1988) Constructing "Gloved" Wings for Aerodynamic Studies. Technical Report NASA TM-100440, Research Engineering, NASA Dryden Flight Research Center.
Burcham, Frank W. and Fullerton, C. Gordon (1991) Controlling Crippled Aircraft–With Throttles. Technical Report NASA TM-104238, 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.
Alag, Gurbux S. and Duke, Eugene L. (1985) Development of a Flight Test Maneuver Autopilot for an F-15 Aircraft. Technical Report NASA TM-86799, 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.
Comperini, Robert and Rhea, Donald C. (1988) Development of an Interactive Real-Time Graphics System for the Display of Vehicle Space Positioning. Technical Report NASA TM-100429, Research Engineering, NASA Dryden Flight Research Center.
Comperini, Robert and Rhea, Donald C. (1988) Development of an Interactive Real-Time Graphics System for the Display of Vehicle Space Positioning. Meeting Paper AIAA-1988-2167, Research Engineering, NASA Dryden Flight Research Center.
Alag, Gurbux Singh and Duke, Eugene L. (1985) Development of Control Laws for a Flight Test Maneuver Autopilot for an F-15 Aircraft. Technical Report NASA TM-86736, 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.
Authors, Various (1984) Digital Electronic Engine Control (DEEC) Flight Evaluation in an F-15 Airplane. Technical Report NASA Conference Publication CP-2298, Research Engineering, NASA Dryden Flight Research Center.
Baer-Riedhart, Jennifer L. (1984) Digital Electronic Engine Control Fault Detection and Accommodation Flight Evaluation.
Putnam, Terrill W. (1984) Digital Electronic Engine Control History.
Curry, Robert E. (1997) Dynamic Ground Effect for a Cranked Arrow Wing Airplane. Meeting Paper AIAA-1997-3649 Research Engineering, NASA Dryden Flight Research Center.
Corda, Stephen and Stephenson, Mark T. and Burcham, Frank W. and Curry, Robert E. (1994) Dynamic Ground Effects Flight Test of an F-15 Aircraft. Technical Report NASA TM-4604, Research Engineering, NASA Dryden Flight Research Center.
Crawford, David B. and Burcham Jr., Frank W. (1984) Effect of Control Logic Modifications on Airstart Performance of F100 Engine Model Derivative Engines in an F-15 Airplane. Technical Report NASA TM-85900, Research Engineering, NASA Dryden Flight Research Center.
Brenner, Martin J. and Iliff, Kenneth W. and Whitman, Robert K. (1978) Effect of Sampling Rate and Record Length on the Determination of Stability and Control Derivatives. Technical Report NASA TM-72858, Research Engineering, NASA Dryden Flight Research Center.
Hughes, Donald L. and Myers, Lawrence P. and Mackall, Karen G. (1985) Effects of Inlet Distortion on a Static Pressure Probe Mounted on the Engine Hub in an F-15 Airplane. Technical Report NASA TP-2411, Research Engineering, NASA Dryden Flight Research Center.
Petersen, Kevin L. (1976) Evaluation of an Envelope-Limiting Device Using Simulation and Flight Test of a Remotely Piloted Research Vehicle. Technical Report NASA Technical Note TN D-8216, Research Engineering, NASA Dryden Flight Research Center.
Duke, Eugene L and Swann, Michael R. and Enevoldson, Einar K. and Wolf, Thomas D. (1983) Experience with Flight Test Trajectory Guidance. Journal of Guidance 6(5):393-398.
Swann, M.R. and Duke, E.L. and Enevoldson, E.K. and Wolf, T.D. (1981) Experience with Flight Test Trajectory Guidance. Meeting Paper AIAA-1981-2504, Research Engineering, NASA Dryden Flight Research Center.
Myers, Lawrence P. (1984) F-15 Digital Electronic Engine Control System Description.
Myers, Lawrence P. and Baer-Riedhart, Jennifer L. and Maxwell, Michael D. (1985) Fault Detection and Accommodation Testing on an F100 Engine in an F-15 Airplane. Technical Report NASA TM-86735, Research Engineering, NASA Dryden Flight Research Center.
Myers, Lawrence P. and Baer-Riedhart, Jennifer L. and Maxwell, Michael D. (1985) Fault Detection and Accommodation Testing on an F100 Engine in an F-15 Airplane. Meeting Paper AIAA-1985-1294, 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.
Burcham, Frank W. and Myers, Lawrence P. and Walsh, Kevin R. (1985) Flight Evaluation of a Digital Electronic Engine Control in an F-15 Airplane. Journal of Aircraft 22(12):1072-1078.
Myers, Lawrence P. and Mackall, Karen G. and Burcham Jr., Frank W. and Walter, Wayne A. (1982) Flight Evaluation of a Digital Electronic Engine Control System in an F-15 Airplane. Meeting Paper AIAA-1982-1080, Research Engineering, NASA Dryden Flight Research Center.
Kurtenbach, Frank J. and Burcham Jr., Frank W. (1981) Flight Evaluation of a Simplified Gross Thrust Calculation Technique Using an F100 Turbofan Engine in an F-15 Airplane. Technical Report NASA TP-1782, Research Engineering, NASA Dryden Flight Research Center.
Burcham Jr., Frank W. and Myers, Lawrence P. (1983) Flight Evaluation of Modifications to a Digital Electronic Engine Control System in an F-15 Airplane. Technical Report NASA TM-83088, Research and Engineering, NASA Dryden Flight Research Center.
Burcham Jr., Frank W. and Myers, Lawrence P. and Zeller, John R. (1983) Flight Evaluation of Modifications to a Digital Electronic Engine Control System in an F-15 Airplane. Meeting Paper AIAA-1983-0537, Research Engineering, NASA Dryden Flight Research Center.
Johnson, J. Blair and Nelson, Jeff (1983) Flight Evaluation of the DEEC Secondary Engine Control Airstart Capability. Technical Report NASA TM-84910, Research Engineering, NASA Dryden Flight Research Center.
Burcham Jr., Frank W. and Myers, Lawrence P. and Walsh, Kevin R. (1983) Flight Evaluation Results for a Digital Electronic Engine Control in an F-15 Airplane. Meeting Paper AIAA-1983-2703, Research Engineering, NASA Dryden Flight Research Center.
Hernandez, Francisco J. and Burcham Jr., Frank W. (1988) Flight Measured and Calculated Exhaust Jet Conditions for an F100 Engine in an F-15 Airplane. Technical Report NASA TM-100419, Research Engineering, NASA Dryden Flight Research Center.
Burken, John and Hanson, Curtis and Lee, James A. and Kaneshige, John (2009) Flight Test Comparison of Different Adaptive Augmentations for Fault Tolerant for a Modified F-15. Meeting Presentation AIAA-2009-2056, Research and Engineering, NASA Dryden Flight Research Center.
Ashworth, George R. and Putnam, Terrill W. and Dana, William J. and Enevoldson, Einar K. and Winter, William R. (1979) Flight Test Evaluation of an RAF High Altitude Partial Pressure Protective Assembly. Technical Report NASA TM-72864, Research Engineering, NASA Dryden Flight Research Center.
Williams-Hayes, Peggy S. (2005) Flight Test Implementation of a Second Generation Intelligent Flight Control System. Technical Report NASA/TM-2005-213669, Research Engineering, NASA Dryden Flight Research Center.
Barrett, W.J. and Rembold, J.P. and Burcham Jr., Frank W. and Myers, Lawrence P. (1981) Flight Test of a Full Authority Digital Electronic Engine Control System in an F-15 Aircraft. Meeting Paper AIAA-1981-1501, Research Engineering, NASA Dryden Flight Research Center.
Antoniewicz, Robert F. and Duke, Eugene L. and Menon, P.K.A. (1990) Flight Test of a Trajectory Controller Using Linearizing Transformations with Measurement Feedback. Meeting Paper AIAA-1990-3373, 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 Paper SFTE2006, Research Engineering, NASA Dryden Flight Research Center.
Burcham Jr., F. W. and Burken, John and Maine, Trindel A. (1994) Flight Testing a Propulsion-Controlled Aircraft Emergency Flight Control System on an F-15 Airplane. Technical Report NASA TM-4590, Research Engineering, NASA Dryden Flight Research Center.
Burcham Jr., Frank W. and Maine, Trindel and Wolf, Thomas (1992) Flight Testing and Simulation of an F-15 Airplane Using Throttles for Flight Control. Technical Report NASA TM-104255, Research Engineering, NASA Dryden Flight Research Center.
Burcham Jr., Frank W. and Maine, Trindel and Wolf, Thomas (1992) Flight Testing and Simulation of an F-15 Airplane Using Throttles for Flight Control. Meeting Paper AIAA-1992-4109, Research Engineering, NASA Dryden Flight Research Center.
Putnam, Terrill W. and Burcham Jr., Frank W. and Kock, Berwin M. (1983) Flight Testing the Digital Electronic Engine Control (DEEC) - A Unique Management Experience.
Myers, Lawrence P. (1984) Flight Testing the Digital Electronic Engine Control in the F-15 Airplane.
Stewart, James F. and Burcham Jr., Frank W. and Gatlin, Donald H. (1992) Flight-Determined Benefits of Integrated Flight-Propulsion Control Systems. Technical Report NASA TM-4393, Research Engineering, NASA Dryden Flight Research Center.
Stewart, James F. and Burcham Jr., Frank W. and Gatlin, Donald H. (1992) Flight-Determined Benefits of Integrated Flight-Propulsion Control Systems. Meeting Paper ICAS 92-2.9.1, Research Engineering, NASA Dryden Flight Research Center.
Plant, Thomas J. and Nugent, Jack and Davis, Robert A. (1980) Flight-Measured Effects of Boattail Angle and Mach Number on the Nozzle Afterbody Flow of a Twin-Jet Fighter. Meeting Paper AIAA-1980-0110, Research Engineering, NASA Dryden Flight Research Center.
Stewart, James F. and Shuck, Thomas L. (1990) Flight-Testing of the Self-Repairing Flight Control System Using the F-15 Highly Integrated Digital Electronic Control Flight Research Facility. Technical Report NASA TM-101725, 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. Meeting Paper AIAA-1998-3872, Research Engineering, NASA Dryden Flight Research Center.
Burcham Jr., Frank W. and Haering Jr., Edward A. (1984) Highly Integrated Digital Engine Control System in an F-15 Airplane. Technical Report NASA TM-86040, Research Engineering, NASA Dryden Flight Research Center.
Ko, William L. (1985) Impacts of Space Shuttle Thermal Protection System Tile on an F-15 Aircraft Vertical Tail. Technical Report NASA TM-85904, Research Engineering, NASA Dryden Flight Research Center.
Meyer Jr., Robert R. and Jarvis, Calvin R. and Barneburg, Jack (1981) In-Flight Aerodynamic Load Testing of the Shuttle Thermal Protection System. Meeting Paper AIAA-1981-2468, 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.
Fisher, David F. and Dougherty Jr., N. Sam (1982) In-Flight Transition Measurement on a 10 Degree Cone at Mach Numbers From 0.5 to 2.0. Technical Report NASA TP-1971, Research Engineering, NASA Dryden Flight Research Center.
Compiled by Holleman, Euclid D. (1974) Initial Results from Flight Testing a Large, Remotely Piloted Airplane Model. Technical Report NASA TM X-56024, Research Engineering, NASA Dryden Flight Research Center.
Hageman, Jacob J. and Smith, Mark S. and Stachowiak, Susan (2003) Integration of Online Parameter Identification and Neural Network for In-Flight Adaptive Control. Technical Report NASA/TM-2003-212028, 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.
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.
Myers, Lawrence P. and Walsh, Kevin R. (1988) Performance Improvements of an F-15 Airplane with an Integrated Engine-Flight Control System. Technical Report NASA TM-100431, Research Engineering, NASA Dryden Flight Research Center.
Sisk, Thomas R. and Matheny, Neil W. (1979) Precision Controllability of the F-15 Airplane. Technical Report NASA TM-72861, Research Engineering, NASA Dryden Flight Research Center.
Webb, Lannie D. and Whitmore, Stephen A. and Janssen, Randall L. (1979) Preliminary Flight and Wind Tunnel Comparisons of the Inlet/Airframe Interaction of the F-15 Airplane. Meeting Paper AIAA-1979-0102, Research Engineering, NASA Dryden Flight Research Center.
Lambert, H.H. and Gilyard, G.B. and Chisholm, J.D. and Kerr, L.J. (1991) Preliminary Flight Evaluation of an Engine Performance Optimization Algorithm. Technical Report NASA TM-4328, Research Engineering, NASA Dryden Flight Research Center.
Cho, Tony K. and Burcham Jr., Frank W. (1984) Preliminary Flight Evaluation of F100 Engine Model Derivative Airstart Capability in an F-15 Airplane. Technical Report NASA TM-86031, 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.
Myers, Lawrence P. and Walsh, Kevin R. (1987) Preliminary Flight Results of an Adaptive Engine Control System on an F-15 Airplane. Meeting Paper AIAA-1987-1847, Research Engineering, NASA Dryden Flight Research Center.
Burcham Jr., Frank W. and Maine, Trindel A. and Fullerton, C. Gordon and Wells, Edward A. (1993) Preliminary Flight Test Results of a Fly-By-Throttle Emergency Flight Control System on an F-15 Airplane. Meeting Paper AIAA-1993-1820, Research Engineering, NASA Dryden Flight Research Center.
Myers, Lawrence P. and Burcham Jr., Frank W. (1984) Preliminary Flight Test Results of the F100 EMD Engine in an F-15 Airplane. Technical Report NASA-TM-85902, Research Engineering, NASA Dryden Flight Research Center.
Myers, Lawrence P. and Burcham Jr., Frank W. (1984) Preliminary Flight Test Results of the F100 EMD Engine in an F-15 Airplane. Meeting Paper AIAA-1984-1332, Research Engineering, NASA Dryden Flight Research Center.
Johnson, J. Blair (1988) Preliminary In-Flight Boundary Layer Transition Measurements on a 45-Degree Swept Wing at Mach Numbers Between 0.9 and 1.8. Technical Report NASA TM-100412, Research Engineering, NASA Dryden Flight Research Center.
Nugent, Jack and Plant, Thomas J. and Davis, Robert A. and Taillon, Norman V. (1983) Pressures Measured in Flight on the Aft Fuselage and External Nozzle of a Twin-Jet Fighter. Technical Report NASA Technical Paper TP-2017, Research Engineering, NASA Dryden Flight Research Center.
Kaneshige, John and Bull, John and Kudzia, Edward and Burcham, Frank W. (1999) Propulsion Control with Flight Director Guidance as an Emergency Flight Control System. Meeting Paper AIAA-1999-3962, Research Engineering, NASA Dryden Flight Research Center.
Burcham Jr., Frank W. and Ray, Ronald J. and Conners, Timothy R. and Walsh, Kevin R. (1998) Propulsion Flight Research at NASA Dryden From 1967 to 1997. Technical Report NASA/TP-1998-206554, Research Engineering, NASA Dryden Flight Research Center.
Burcham Jr., Frank W. and Ray, Ronald J. and Conners, Timothy R. and Walsh, Kevin R. (1998) Propulsion Flight Research at NASA Dryden from 1967 to 1997. Meeting Paper AIAA-1998-3712, Research Engineering, NASA Dryden Flight Research Center.
Burcham Jr., Frank W. and Gilyard, Glenn B. and Myers, Lawrence P. (1990) Propulsion System-Flight Control Integration-Flight Evaluation and Technology Transition. Meeting Paper AIAA-1990-2280, Research Engineering, NASA Dryden Flight Research Center.
Burcham Jr., Frank W. and Gilyard, Glenn B. and Myers, Lawrence P. (1990) Propulsion System/Flight Control Integration and Optimization—Flight Evaluation and Technology Transition. Technical Report NASA TM-4207, Research Engineering, NASA Dryden Flight Research Center.
Smith, Mark S. and Moes, Timothy R. and Morelli, Eugene A. (2003) Real-Time Stability and Control Derivative Extraction From F-15 Flight Data. Technical Report NASA/TM-2003-212027, Research Engineering, NASA Dryden Flight Research Center.
Burcham Jr., Frank W. and Myers, Lawrence P. and Nugent, Jack and Lasagna, Paul L. and Webb, Lannie D. (1981) Recent Propulsion System Flight Tests at the NASA Dryden Flight Research Center. Meeting Paper AIAA-1981-2438, Research Engineering, NASA Dryden Flight Research Center.
Burken, John J. and Williams-Hayes, Peggy and Kaneshige, John T. and Stachowiak, Susan J. (2006) Reconfigurable Control with Neural Network Augmentation for a Modified F-15 Aircraft. Technical Report NASA/TM-2006-213678, Research Engineering, NASA Dryden Flight Research Center.
Stevens, C.H. and Spong, E.D. and Nugent, Jack and Neumann, H.E. (1979) Reynolds Number, Scale and Frequency Content Effects on F-15 Inlet Instantaneous Distortion. Meeting Paper AIAA-1979-0104, Research Engineering, NASA Dryden Flight Research Center.
Williams-Hayes, Peggy S. (2004) Selected Flight Test Results for Online Learning Neural Network-Based Flight Control System. Technical Report NASA/TM-2004-212857, Research Engineering, NASA Dryden Flight Research Center.
Williams, Peggy S. (2004) Selected Flight Test Results for Online Learning Neural Network-Based Flight Control System. Meeting Paper AIAA-2004-6283, 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.
Webb, Lannie D. and Nugent, Jack (1982) Selected Results of the F-15 Propulsion Interactions Program. Meeting Paper AIAA-1982-1041, Research Engineering, NASA Dryden Flight Research Center.
Burcham Jr., Frank W. and Maine, Trindel A. and Kaneshige, John and Bull, John (1999) Simulator Evaluation of Simplified Propulsion-Only Emergency Flight Control Systems on Transport Aircraft. Technical Report NASA/TM-1999-206578, 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 and 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. Meeting Paper AIAA-1992-3743, 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. Meeting Paper AIAA-1992-3745 Research Engineering, NASA Dryden Flight Research Center.
Iliff, Kenneth W. and Maine, Richard E. and Shafer, Mary F. (1976) Subsonic Stability and Control Derivatives for an Unpowered, Remotely Piloted 3/8-Scale F-15 Airplane Model Obtained From Flight Test. Technical Report NASA Technical Note TN D-8136, Research Engineering, NASA Dryden Flight Research Center.
Holleman, Euclid C. (1976) Summary of Flight Tests to Determine the Spin and Controllability Characteristics of a Remotely Piloted, Large-Scale (3/8) Fighter Airplane Model. Technical Report NASA Technical Note TN D-8052, Research Engineering, NASA Dryden Flight Research Center.
Burcham Jr., Frank W. and Trippensee, Gary A. and Fisher, David F. and Putnam, Terrill W. (1986) Summary of Results of NASA F-15 Flight Research Program. Technical Report NASA TM-86811, Research Engineering, NASA Dryden Flight Research Center.
Burcham Jr., Frank W. and Trippensee, Gary A. and Fisher, David F. and Putnam, Terrill W. (1986) Summary of Results of NASA F-15 Flight Research Program. Meeting Paper AIAA-1986-9761, Research Engineering, NASA Dryden Flight Research Center.
Bohn-Meyer, Marta and Jiran, Fred (1981) Techniques for Modifying Airfoils and Fairings on Aircraft Using Foam and Fiberglass. Conference Paper AIAA-1981-2445, Research Engineering, NASA Dryden Flight Research Center.
Bever, Glenn A. (1984) The Development of an Airborne Instrumentation Computer System for Flight Test. Technical Report NASA TM-86036, Research Engineering, NASA Dryden Flight Research Center.
Evans, Alison B. (1991) The Effects of Compressor Seventh-Stage Bleed Air Extraction on Performance of the F100-PW-220 Afterburning Turbofan Engine. Technical Report NASA CR-179447, Research Engineering, NASA Dryden Flight Research Center.
Moore, Archie L. (1986) The Role of a Real-Time Flight Support Facility in Flight Research Programs. Technical Report NASA TM-86805, Research Engineering, NASA Dryden Flight Research Center.
Moore, Archie L. (1986) The Role of a Real-Time Flight Support Facility in Flight Research Programs. Meeting Paper AIAA-1986-0166, Research Engineering, NASA Dryden Flight Research Center.
Burcham Jr., Frank W. and Ray, Ronald J. (1987) The Value of Early Flight Evaluation of Propulsion Concepts Using the NASA F-15 Research Airplane. Technical Report NASA TM-100408, Research Engineering, NASA Dryden Flight Research Center.
Burcham Jr., Frank W. and Ray, Ronald J. (1987) The Value of Early Flight Evaluation of Propulsion Concepts Using the NASA F-15 Research Airplane. Meeting Paper AIAA-1987-2877, Research Engineering, NASA Dryden Flight Research Center.
Conners, Timothy R. (1992) Thrust Stand Evaluation of Engine Performance Improvement Algorithms in an F-15 Airplane. Meeting Paper AIAA-1992-3747, 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.
Burcham Jr., Frank W. and Maine, Trindel A. and Burken, John J. and Bull, John (1998) Using Engine Thrust for Emergency Flight Control: MD-11 and B-747 Results. Technical Report NASA/TM-1998-206552, Research Engineering, NASA Dryden Flight Research Center.
Lorincz, Dale J. and Friend, Edward L. (1979) Water Tunnel Visualization of the Vortex Flows of the F-15. Meeting Paper AIAA-1979-1649, Research Engineering, NASA Dryden Flight Research Center.
This list was generated on Fri Nov 6 18:16:22 PST 2009.
