Subject: (01) Aeronautics - General
Number of records: 65.
Marshall, Laurie A. and Corpening, Griffin P. and Sherrill, Robert (2005) A Chief Engineer's View of the NASA X-43A Scramjet Flight Test. Conference Presentation AIAA-2005-3332, Research Engineering, NASA Dryden Flight Research Center.
Smith, Harriet J. (1975) A Flight Test Investigation of The Rolling Moments Induced on a T-37B Airplane in The Wake of a B-747 Airplane. Technical Report NASA TM X-56031, Research Engineering, NASA Dryden Flight Research Center.
Jenkins, Jerald M. and Quinn, Robert D. (1996) A Historical Perspective of the YF-12A Thermal Loads and Structures Program. Technical Report NASA TM-104317, Research Engineering, NASA Dryden Flight Research Center.
Sisk, Thomas R. and Matheny, Neil W. and Kier, David A. and Manke, John A. (1968) A Preliminary Flying-Qualities Evaluation of a Variable-Sweep Fighter-Type Aircraft. Technical Report NASA TM X-1583, Research Engineering, NASA Dryden Flight Research Center.
Wall, Douglas E. (1964) A Study of Hypersonic Aircraft. Technical Report NASA TM X-56001, Research Engineering, NASA Dryden Flight Research Center.
Jenkins, Jerald M. and DeAngelis, V. Michael (1997) A Summary of Numerous Strain-Gage Load Calibrations on Aircraft Wings and Tails in a Technological Format. Technical Report NASA TM-4804, Research Engineering, NASA Dryden Flight Research Center.
Lasagna, Paul and Mackall, Karen (1981) Acoustic Flight Testing of Advanced Design Propellers on a JetStar Aircraft. Conference Paper, NASA Conference Publication 2208, Research Engineering, NASA Dryden Flight Research Center.
Authors, Various (1976) Advanced Control Technology and Its Potential for Future Transport Aircraft. Technical Report NASA TM X-3409, Research Engineering, NASA Dryden Flight Research Center.
Noll, Richard B. and Jarvis, Calvin R. and Pembo, Chris and Lock, Wilton P. and Scott, Betty J. (1963) Aerodynamic and Control-System Contributions to the X-15 Airplane Landing-Gear Loads. Technical Report NASA Technical Note TN D-2090, Research Engineering, NASA Dryden Flight Research Center.
Brenner, Marty and Prazenica, Chad (2005) Aeroelastic Flight Data Analysis with the Hilbert-Huang Algorithm. Meeting Paper AIAA-2005-5917, Research Engineering, NASA Dryden Flight Research Center.
Brenner, Martin J. and Prazenica, Chad (2006) Aeroelastic Flight Data Analysis with the Hilbert–Huang Algorithm. Technical Report NASA/TM-2006-213665, Research Engineering, NASA Dryden Flight Research Center.
Weil, Joseph and Day, Richard E. (1956) An Analog Study of the Relative Importance of Various Factors Affecting Roll Coupling. Technical Report NACA RM H56A06, Research Engineering, NASA Dryden Flight Research Center.
Hedgley Jr., David R. (1976) An Exact Transformation from Geocentric to Geodetic Coordinates for Nonzero Altitudes. NASA Technical Report TR R-458, Research Engineering, NASA Dryden Flight Research Center.
Walker, Harold J. (1981) Analytic Study of Orbiter Landing Profiles. Technical Report NASA TM-81365, Research Engineering, NASA Dryden Flight Research Center.
Authors, Various (1980) Annual Report on Research and Technology Accomplishments. Technical Report NASA-TM-102949, Research Engineering, NASA Dryden Flight Research Center.
Saltzman, Edwin J. (1964) Base Pressure Coefficients Obtained from the X-15 Airplane for Mach Numbers up to 6. Technical Report NASA Technical Note TN D-2420, Research Engineering, NASA Dryden Flight Research Center.
Larson, Terry J. and Webb, Lannie D. (1963) Calibrations and Comparisons of Pressure-Type Airspeed-Altitude Systems of the X-15 Airplane from Subsonic to High Supersonic Speeds. Technical Report NASA Technical Note TN D-1724, Research Engineering, NASA Dryden Flight Research Center.
Bui, Trong T. (2009) CFD Analysis of Nozzle Jet Plume Effects on Sonic Boom Signature. Technical Report NASA/TM-2009-214650, Research and Engineering, NASA Dryden Flight Research Center.
Bui, Trong T. (2009) CFD Analysis of Nozzle Jet Plume Effects on Sonic Boom Signature. Meeting Paper AIAA-2009-1054, Research and Engineering, NASA Dryden Flight Research Center.
Banas, Ronald P. (1965) Comparison of Measured and Calculated Turbulent Heat Transfer in a Uniform and Nonuniform Flow Field on the X-15 Upper Vertical Fin at Mach Numbers of 4.2 and 5.3. Technical Report NASA TM X-1136, Research Engineering, NASA Dryden Flight Research Center.
Jenkins, Jerald M. and Schuster, Lawrence S. and Carter, Alan L. (1978) Correlation of Predicted and Measured Thermal Stresses on a Truss-Type Aircraft Structure. Technical Report NASA TM-72857, Research Engineering, NASA Dryden Flight Research Center.
Jenkins, Jerald M. (1979) Correlation of Predicted and Measured Thermal Stresses on an Advanced Aircraft Structure with Dissimilar Materials. Technical Report NASA TM-72865, Research Engineering, NASA Dryden Flight Research Center.
Jenkins, Jerald M. (1979) Correlation of Predicted and Measured Thermal Stresses on an Advanced Aircraft Structure with Similar Materials. Technical Report NASA TM-72862, 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.
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.
Gilyard, Glenn (1996) Development of a Real-Time Transport Performance Optimization Methodology. Technical Report NASA TM-4730, Research Engineering, NASA Dryden Flight Research Center.
Gupta, K.K. and Brenner, M.J. and Voelker, L.S. (1991) Development of an Integrated Aeroservoelastic Analysis Program and Correlation With Test Data. Technical Report NASA Technical Paper TP-3120, Research Engineering, NASA Dryden Flight Research Center.
Jenkins, Jerald M. (1979) Effect of Element Density on the NASTRAN Calculated Mechanical and Thermal Stresses of a Spar. Technical Report NASA TM-72868, Research Engineering, NASA Dryden Flight Research Center.
Montoya, Lawrence C. and Steers, Louis L. and Christopher, David and Trujillo, Bianca (1981) F-111 TACT Natural Laminar Flow Glove Flight Results. Conference Paper, NASA Conference Publication 2208, Research Engineering, NASA Dryden Flight Research Center.
Taylor Jr., Lawrence W. and Iliff, Kenneth W. (1969) Fixed-Base Simulator Pilot Rating Surveys for Predicting Lateral-Directional Handling Qualities and Pilot Rating Variability. Technical Report NASA Technical Note TN D-5358, Research Engineering, NASA Dryden Flight Research Center.
Powers, Bruce G. and Matheny, Neil W. (1964) Flight Evaluation of Three Techniques of Demonstrating the Minimum Flying Speed of a Delta-Wing Airplane. Technical Report NASA Technical Note TN D-2337, Research Engineering, NASA Dryden Flight Research Center.
Drake, Hubert M. (1956) Flight Experience with Present Research Airplanes. Technical Report NACA-CONF-26-Oct-56-p15-22, Research Engineering, NASA Dryden Flight Research Center.
Holleman, Euclid C. (1970) Flight Investigation of the Roll Requirements for Transport Airplanes in Cruising Flight. Technical Report NASA Technical Note TN D-5957, Research Engineering, NASA Dryden Flight Research Center.
Jenkins, Jerald M. and DeAngelis, V. Michael and Friend, Edward L. and Monaghan, Richard C. (1969) Flight Measurements of Canard Loads, Canard Buffeting, and Elevon and Wing-Tip Hinge Moments on the XB-70 Aircraft Including Comparisons with Predictions. Technical Report NASA Technical Note TN D-5359, Research Engineering, NASA Dryden Flight Research Center.
Gilyard, Glenn B. and Belte, Daumants (1974) Flight-Determined Lag of Angle-of-Attack and Angle-of-Sideslip Sensors in the YF-12A Airplane from Analysis of Dynamic Maneuvers. Technical Report NASA Technical Note TN D-7819, Research Engineering, NASA Dryden Flight Research Center.
Taillon, Norman V. (1974) Flight-Test Investigation of the Aerodynamic Characteristics and Flow Interference Effects about the Aft Fuselage of the F-111A Airplane. Technical Report NASA Technical Note TN D-7563, Research Engineering, NASA Dryden Flight Research Center.
Jarvis, Calvin R. and Szalai, Kenneth J. (1981) Ground and Flight Test Experience with a Triply Redundant Digital Fly-By-Wire Control System. Conference Paper, NASA Conference Publication 2172, Research Engineering, NASA Dryden Flight Research Center.
Watts, Joe D. and Olinger, Frank V. (1968) Heat-Transfer Effects of Surface Protuberances on the X-15 Airplane. Technical Report NASA TM X-1566, Research Engineering, NASA Dryden Flight Research Center.
Ehernberger, L. J. and Love, Betty J. (1975) High Altitude Gust Acceleration Environment as Experienced by a Supersonic Airplane. Technical Report NASA Technical Note TN D-7868, Research Engineering, NASA Dryden Flight Research Center.
Montoya, Lawrence C. (1981) KC-135 Winglet Flight Results. Conference Paper, NASA Conference Publication 2172, Research Engineering, NASA Dryden Flight Research Center.
Lasagna, Paul L. and Mackall, Karen G. and Burcham Jr., Frank W. and Putnam, Terrill W. (1980) Landing Approach Airframe Noise Measurements and Analysis. Technical Report NASA TP-1602, Research Engineering, NASA Dryden Flight Research Center.
Allen, Michael J. and Lizotte, Andrew M. and Dibley, Ryan P. and Clarke, Robert (2005) Loads Model Development and Analysis for the F/A-18 Active Aeroelastic Wing Airplane. Technical Report NASA/TM-2005-213663, Research Engineering, NASA Dryden Flight Research Center.
Allen, Michael J. and Lizotte, Andrew M. and Dibley, Ryan P. and Clarke, Robert (2005) Loads Model Development and Analysis for the F/A-18 Active Aeroelastic Wing Airplane. Conference Presentation AIAA-2005-6313, Research Engineering, NASA Dryden Flight Research Center.
Pak, Chan-gi and Li, Wesley (2008) Multidisciplinary Design, Analysis, and Optimization Tool Development Using a Genetic Algorithm. Meeting Paper ICAS 2008-1.1.1, Research and Engineering, NASA Dryden Flight Research Center.
Steers, Louis L. (1981) Natural Laminar Flow Flight Experiment. Conference Paper, NASA Conference Publication 2172, Research Engineering, NASA Dryden Flight Research Center.
Bui, Trong T. and Lux, David P. and Stenger, Michael T. and Munson, Michael J. and Teate, George F. (2007) New Air-Launched Small Missile (ALSM) Flight Testbed for Hypersonic Systems. Technical Report NASA/TM-2007-214624, Research and Engineering, NASA Dryden Flight Research Center.
Bui, Trong T. and Lux, David P. and Stenger, Michael T. and Munson, Michael J. and Teate, George F. (2006) New Air-Launched Small Missile (ALSM) Flight Testbed for Hypersonic Systems. Meeting Paper AIAA-2006-221, Research Engineering, NASA Dryden Flight Research Center.
Painter, Weneth D. and Kock, Berwin M. (1969) Operational Experiences and Characteristics of the M2-F2 Lifting Body Flight Control System. Technical Report NASA TM X-1809, Research Engineering, NASA Dryden Flight Research Center.
Marshall, Laurie A. and Bahm, Catherine and Corpening, Griffin P. and Sherrill, Robert (2005) Overview With Results and Lessons Learned of the X-43A Mach 10 Flight. Conference Presentation AIAA-2005-3336, Research Engineering, NASA Dryden Flight Research Center.
Walker, Harold J. (1979) Performance Evaluation Method for Dissimilar Aircraft Designs. Technical Report NASA Reference Publication RP-1042, Research Engineering, NASA Dryden Flight Research Center.
Smith, Mark S. (2006) Photogrammetric Trajectory Estimation of Foam Debris Ejected From an F-15 Aircraft. Technical Report NASA/TM-2006-213675, Research Engineering, NASA Dryden Flight Research Center.
Gong, Leslie and Richards, W. Lance and Monaghan, Richard C. and Quinn, Robert D. (1993) Preliminary Analysis for a Mach 8 Crossflow Transition Experiment on the Pegasus® Space Booster. Technical Report NASA TM-104272, Research Engineering, NASA Dryden Flight Research Center.
Jenkins, Jerald M. and Lemcoe, M. M. (1977) Problems Associated with Attaching Strain Gages to Titanium Alloy Ti-6Al-4V. Technical Report NASA TM X-56044, Research Engineering, NASA Dryden Flight Research Center.
Stillwell, Wendell H. (1955) Results of Measurements Made During the Approach and Landing of Seven High-Speed Research Airplanes. Technical Report NACA RM H54K24, 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.
Lung, Shun-fat and Pak, Chan-gi (2008) Structural Model Tuning Capability in an Object-Oriented Multidisciplinary Design, Analysis, and Optimization Tool. Technical Report NASA/TM-2008-214640, Research and Engineering, NASA Dryden Flight Research Center.
Lung, Shun-fat and Pak, Chan-gi (2008) Structural Model Tuning Capability in an Object-Oriented Multidisciplinary Design, Analysis, and Optimization Tool. Meeting paper ICAS 2008-9.5.1, Research and 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.
Bauer, Jeff (2007) The NASA Dryden Flight Research Center Unmanned Aircraft System Service Capabilities. Technical Report NASA/TM-2007-214619, Research and Engineering, NASA Dryden Flight Research Center.
Bauer, Jeff (2007) The NASA Dryden Flight Research Center Unmanned Aircraft System Service Capabilities. Conference Paper UAV2007BAUER, Research and Engineering, NASA Dryden Flight Research Center.
Lung, Shun-fat and Pak, Chan-gi (2009) Updating the Finite Element Model of the Aerostructures Test Wing Using Ground Vibration Test Data. Technical Report NASA/TM-2009-214646, Research and Engineering, NASA Dryden Flight Research Center.
Conley, Joseph L. (1992) User's Manual for AeroFcn: A FORTRAN Program to Compute Aerodynamic Parameters. Technical Report NASA TM-104237, Research Engineering, NASA Dryden Flight Research Center.
Adkins, Elmor J. and McLeod, Norman J. and Lasagna, Paul L. (1969) Variation in Engine Noise for Two Landing-Approach Configurations of a Jet Transport Aircraft. Technical Report NASA TM X-1896, Research Engineering, NASA Dryden Flight Research Center.
This list was generated on Sun Nov 22 18:15:14 PST 2009.
