Subject: (02) Aerodynamics
Number of records: 186.
Bowers, Albion H. and Sim, Alex G. (1984) A Comparison of Wortmann Airfoil Computer-Generated Lift and Drag Polars With Flight and Wind Tunnel Results. Technical Report NASA TM-86035, Research Engineering, NASA Dryden Flight Research Center.
Whitmore, Stephen A. and Petersen, Brian J. and Scott, David D. (1996) A Dynamic Response Model for Pressure Sensors in Continuum and High Knudsen Number Flows with Large Temperature Gradients. Technical Report NASA TM-4728, Research Engineering, NASA Dryden Flight Research Center.
Diebler, Corey and Smith, Mark (2002) A Ground-Based Research Vehicle for Base Drag Studies at Subsonic Speeds. Technical Report NASA/TM-2002-210737, Research Engineering, NASA Dryden Flight Research Center.
Taillon, Norman V. (1968) A Method for the Surface Installation and Fairing of Static-Pressure Orifices on a Large Supersonic-Cruise Airplane. Technical Report NASA TM X-1530, Research Engineering, NASA Dryden Flight Research Center.
Saltzman, Edwin J. and Meyer Jr., Robert R. (1999) A Reassessment of Heavy-Duty Truck Aerodynamic Design Features and Priorities. Technical Report NASA/TP-1999-206574, Research Engineering, NASA Dryden Flight Research Center.
Larson, Terry J. and Schweikhard, William G. (1974) A Simplified Flight-Test Method For Determining Aircraft Takeoff Performance That Includes Effects of Pilot Technique. Technical Report NASA Technical Note TN D-7603, Research Engineering, NASA Dryden Flight Research Center.
Bjarke, Lisa J. and Del Frate, John H. and Fisher, David F. (1992) A Summary of the Forebody High-Angle-of-Attack Aerodynamics Research on the F-18 and the X-29A Aircraft. Technical Report NASA TM-104261, Research Engineering, NASA Dryden Flight Research Center.
Diebler, Corey G. and Cumming, Stephen B. (2005) Active Aeroelastic Wing Aerodynamic Model Development and Validation for a Modified F/A-18A Airplane. Technical Report NASA/TM-2005-213668, Research Engineering, NASA Dryden Flight Research Center.
Cumming, Stephen B. and Diebler, Corey G. (2005) Active Aeroelastic Wing Aerodynamic Model Development and Validation for a Modified F/A-18A. Meeting Paper AIAA-2005-6312, Research Engineering, NASA Dryden Flight Research Center.
Saltzman, Edwin J. and Wang, K. Charles and Iliff, Kenneth W. (2002) Aerodynamic Assessment of Flight-Determined Subsonic Lift and Drag Characteristics of Seven Lifting-Body and Wing-Body Reentry Vehicle Configurations. Technical Report NASA/TP-2002-209032, Research Engineering, NASA Dryden Flight Research Center.
Maine, Richard E. (1978) Aerodynamic Derivatives for an Oblique Wing Aircraft Estimated From Flight Data by Using a Maximum Likelihood Technique. Technical Report NASA TP-1336, Research Engineering, NASA Dryden Flight Research Center.
Steers, Louis L. and Montoya, Lawrence C. and Saltzman, Edwin J. (1975) Aerodynamic Drag Reduction Tests on a Full-Scale Tractor-Trailer Combination and a Representative Box-Shaped Ground Vehicle. Conference Paper SAE 750703, Research Engineering, NASA Dryden Flight Research Center.
Montoya, Lawrence C. and Steers, Louis L. (1974) Aerodynamic Drag Reduction Tests on a Full-Scale Tractor-Trailer Combination with Several Add-On Devices. Technical Report NASA TM X-56028, Research Engineering, NASA Dryden Flight Research Center.
Cumming, Stephen B. and Smith, Mark S. and Frederick, Michael A. (2008) Aerodynamic Effects of a 24-Foot Multisegmented Telescoping Nose Boom on an F-15B Airplane. Technical Report NASA/TM-2008-214634, Research and Engineering, NASA Dryden Flight Research Center.
Cumming, Stephen B. and Smith, Mark S. and Frederick, Michael A. (2007) Aerodynamic Effects of a 24-Foot, Multisegmented Telescoping Nose Boom on an F-15B Airplane. Conference Paper AIAA-2007-6638, Research and Engineering, NASA Dryden Flight Research Center.
Lin, Jensen and Iliff, Kenneth W. (2000) Aerodynamic Lift and Moment Calculations Using a Closed-Form Solution of the Possio Equation. Technical Report NASA/TM-2000-209019, Research Engineering, NASA Dryden Flight Research Center.
Kukreja, Sunil L. (2007) Aeroelastic Model Structure Computation for Envelope Expansion. Technical Report NASA/TM-2007-214623, Research and Engineering, NASA Dryden Flight Research Center.
Banks, Daniel W. and Fisher, David F. (2006) Aft-End Flow of a Large-Scale Lifting Body During Free-Flight Tests. Technical Report NASA/TM-2006-213681, Research Engineering, NASA Dryden Flight Research Center.
Banks, Daniel W. and Fisher, David F. (2006) Aft-End Flow of a Large-Scale Lifting Body During Free-Flight Tests. Meeting Paper ISFV12, Research Engineering, NASA Dryden Flight Research Center.
Curry, Robert E. and Moulton, Bryan J. and Kresse, John (1989) An In-Flight Investigation of Ground Effect on a Forward-Swept Wing Airplane. Technical Report NASA TM-101708, Research Engineering, NASA Dryden Flight Research Center.
Marcy, William L. and Stephenson, Harriet J. and Cooney, Thomas V. (1956) Analysis of the Vertical-Tail Loads Measured During a Flight Investigation at Transonic Speeds of the Douglas X-3 Research Airplane. Technical Report NACA RM H56H08, Research Engineering, NASA Dryden Flight Research Center.
Shubov, Marianna A. and Peterson, Cheryl A. (2003) Asymptotic Distribution of Eigenfrequencies for a Coupled Euler-Bernoulli and Timoshenko Beam Model. Technical Report NASA/CR-2003-212022, Research Engineering, NASA Dryden Flight Research Center.
Marshall, Laurie A. (1999) Boundary-Layer Transition Results From the F-16XL-2 Supersonic Laminar Flow Control Experiment. Technical Report NASA/TM-1999-209013, Research Engineering, NASA Dryden Flight Research Center.
DeAngelis, V. Michael and Monaghan, Richard C. (1977) Buffet Characteristics of the F-8 Supercritical Wing Airplane. Technical Report NASA TM-56049, Research Engineering, NASA Dryden Flight Research Center.
Balakrishnan, A.V. and Edwards, John W. (1980) Calculation of the Transient Motion of Elastic Airfoils Forced by Control Surface Motion and Gusts. Technical Report NASA TM-81351, Research Engineering, NASA Dryden Flight Research Center.
Johnson, J. Blair and Sandlin, Doral R. (1986) Comparison of Theoretical and Flight-Measured Local Flow Aerodynamics for a Low-Aspect-Ratio Fin. Technical Report NASA TM-86806, Research Engineering, NASA Dryden Flight Research Center.
Teets Jr., Edward H. and Harvey, Philip O. (2000) Comparison of Three Wind Measuring Systems for Flight Test. Meeting Paper AMS Paper P1.4, Research Engineering, NASA Dryden Flight Research Center.
Nugent, Jack and Pendergraft Jr., Odis C. (1987) Comparison of Wind Tunnel and Flight Test Afterbody and Nozzle Pressures for a Twin-Jet Fiqhter Aircraft at Transonic Speeds. Technical Report NASA TP-2588, Research Engineering, NASA Dryden Flight Research Center.
Montoya, Lawrence C. and Lux, David P. (1975) Comparisons of Wing Pressure Distribution from Flight Tests of Flush and External Orifices for Mach Numbers from 0.50 to 0.97. Technical Report NASA TM X-56032, Research Engineering, NASA Dryden Flight Research Center.
Larson, Terry J. (1974) Compensated and Uncompensated Nose Boom Static Pressures Measured from Two Air Data Systems on a Supersonic Airplane. Technical Report NASA TM X-3132, Research Engineering, NASA Dryden Flight Research Center.
Cosentino, Gary B. (2008) Computational Fluid Dynamics Analysis Success Stories of X-plane Design on Flight Test. Technical Report NASA/TM-2008-214636, Research and 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.
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.
Fisher, David F. and Richwine, David M. and Landers, Stephen (1992) Correlation of Forebody Pressures and Aircraft Yawing Moments on the X-29A Aircraft at High Angles of Attack. Technical Report NASA TM-4417, Research Engineering, NASA Dryden Flight Research Center.
Authors, Various (1975) Description and Flight Test Results of the NASA F-8 Digital Fly-By-Wire Control System. Technical Report NASA Technical Note TN D-7843, Research Engineering, NASA Dryden Flight Research Center.
Yuhas, Andrew J. and Ray, Ronald J. and Burley, Richard R. and Steenken, William G. and Lechtenberg, Leon and Thornton, Don (1995) Design and Development of an F/A-18 Inlet Distortion Rake: A Cost and Time Saving Solution. Technical Report NASA TM-4722, Research Engineering, NASA Dryden Flight Research Center.
Bui, Trong T. and Oates, David L. and Gonsalez, Jose C. (2000) Design and Evaluation of a New Boundary-Layer Rake for Flight Testing. Technical Report NASA/TM-2000-209014, Research Engineering, NASA Dryden Flight Research Center.
Bui, Trong T. and Oates, David L. and Gonsalez, Jose C. (2000) Design and Evaluation of a New Boundary-Layer Rake for Flight Testing. Meeting Paper AIAA-2000-0503, 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.
Painter, Weneth D. and Caw, Lawrence J. (1979) Design and Physical Characteristics of the Transonic Aircraft Technology (TACT) Research Aircraft. Technical Report NASA TM-56048, Research Engineering, NASA Dryden Flight Research Center.
Greer, Donald and Hamory, Phil and Krake, Keith and Drela, Mark (1999) Design and Predictions for a High-Altitude (Low-Reynolds Number) Aerodynamic Flight Experiment. Technical Report NASA/TM-1999-206579, Research Engineering, NASA Dryden Flight Research Center.
Greer, Donald and Hamory, Phil and Krake, Keith and Drela, Mark (1999) Design and Predictions for a High-Altitude (Low-Reynolds-Number) Aerodynamic Flight Experiment. Meeting Paper AIAA-1999-3183, Research Engineering, NASA Dryden Flight Research Center.
Greer, Donald and Hamory, Phil and Krake, Keith and Drela, Mark (2000) Design and Predictions for High-Altitude (Low Reynolds Number) Aerodynamic Flight Experiment. Journal of Aircraft 37(4):684-689.
Fisher, David F. and Haering Jr., Edward A. and Noffz, Gregory K. and Aguilar, Juan I. (1998) Determination of Sun Angles for Observations of Shock Waves on a Transport Aircraft. Technical Report NASA/TM-1998-206551, Research Engineering, NASA Dryden Flight Research Center.
Richwine, David M. and Del Frate, John H. (1994) Development of a Low-Aspect Ratio Fin for Flight Research Experiments. Technical Report NASA TM-4596, 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.
Cobleigh, Brent R. (1998) Development of the X-33 Aerodynamic Uncertainty Model. Technical Report NASA/TP-1998-206544, Research Engineering, NASA Dryden Flight Research Center.
Speer, Steven E. and Zhong, Xiaolin and Gong, Leslie and Quinn, Robert (2004) DNS of Attachment-Line/Crossflow Boundary Layer Instability in Supersonic Swept Wing Flows. Meeting Paper AIAA-2004-252, Research Engineering, NASA Dryden Flight Research Center.
Saltzman, Edwin J. and Meyer Jr., Robert R. (1974) Drag Reduction Obtained by Rounding Vertical Corners on a Box-Shaped Ground Vehicle. Technical Report NASA TM X-56023, Research Engineering, NASA Dryden Flight Research Center.
Peterson, Randall L. (1981) Drag Reduction Obtained by the Addition of a Boattail to a Box Shaped Vehicle. Technical Report NASA CR-163113, Research Engineering, NASA Dryden Flight Research Center.
Curry, Robert E. (1997) Dynamic Ground Effect for a Cranked Arrow Wing Airplane. Technical Report NASA TM-4799, 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.
Fisher, David F. and Murri, Daniel G. and Lanser, Wendy R. (1996) Effect of Actuated Forebody Strakes on the Forebody Aerodynamics of the NASA F-18 HARV. Technical Report NASA TM-4774, Research Engineering, NASA Dryden Flight Research Center.
Matthews Jr., James T. (1948) Effect of Downwash on the Estimated Elevator Deflection Required for Trim of the XS-1 Airplane at Supersonic Speeds. Technical Report NACA RM L8H06a, Research Engineering, NASA Dryden Flight Research Center.
Monaghan, Richard C. and Friend, Edward L. (1973) Effects of Flaps on Buffet Characteristics and Wing-Rock Onset of an F-8C Airplane at Subsonic and Transonic Speeds. Technical Report NASA TM X-2873, Research Engineering, NASA Dryden Flight Research Center.
Meyer Jr., Robert R. and Covell, Peter F. (1986) Effects of Winglets on a First-Generation Jet Transport Wing. VII - Sideslip Effects on Winglet Loads and Selected Wing Loads at Subsonic Speeds for a Full-Span Model. Technical Report NASA TP-2619, 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.
Bolonkin, Alexander and Gilyard, Glenn B. (1999) Estimated Benefits of Variable-Geometry Wing Camber Control for Transport Aircraft. Technical Report NASA/TM-1999-206586, Research Engineering, NASA Dryden Flight Research Center.
Bennett, Donald L. (1975) Evaluation of a Hemispherical Head Flow Direction Sensor for Inlet Duct Measurements. Technical Report NASA TM X-3232, Research Engineering, NASA Dryden Flight Research Center.
Smith, Harriet J. (1965) Evaluation of the Lateral-Directional Stability and Control Characteristics of the Lightweight M2-F1 Lifting Body at Low Speeds. Technical Report NASA Technical Note TN D-3022, Research Engineering, NASA Dryden Flight Research Center.
Wolowicz, Chester H. and Yancey, Roxanah B. (1974) Experimental Determination of Airplane Mass and Inertial Characteristics. Technical Report NASA TR R-433, Research Engineering, NASA Dryden Flight Research Center.
Durgesh, V. and Naughton, J. W. and Whitmore, S. A. (2004) Experimental Investigation of Base Drag Reduction on a Two-Dimensional Body Using Boundary Layer Manipulation. Meeting Paper AIAA-2004-904, 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.
Kukreja, Sunil L. (2007) F-15B Quiet Spike™ Aeroservoelastic Flight-Test Data Analysis. Technical Report NASA/TM-2007-214618, Research and Engineering, NASA Dryden Flight Research Center.
Richwine, David. M. (1996) F-15B/Flight Test Fixture II: A Test Bed for Flight Research. Technical Report NASA TM-4782, Research Engineering, NASA Dryden Flight Research Center.
Landers, Stephen F. and Saltzman, John A. and Bjarke, Lisa J. (1997) F-16XL Wing Pressure Distributions and Shock Fence Results from Mach 1.4 to Mach 2.0. Technical Report NASA/TM-97-206219, Research Engineering, NASA Dryden Flight Research Center.
Fisher, David F. and Banks, Daniel W. and Richwine, David M. (1990) F-18 High Alpha Research Vehicle Surface Pressures: Initial In-Flight Results and Correlation With Flow Visualization and Wind-Tunnel Data. Technical Report NASA TM-101724, Research Engineering, NASA Dryden Flight Research Center.
Montoya, Lawrence C. and Banner, Richard D. (1977) F-8 Supercritical Wing Flight Pressure, Boundary-Layer, and Wake Measurements and Comparisons with Wind Tunnel Data. Technical Report NASA TM X-3544, Research Engineering, NASA Dryden Flight Research Center.
Tang, Ming H. and DeAngelis, V. Michael (1969) Fin Loads and Control-Surface Hinge Moments Measured in Full-Scale Wind-Tunnel Tests on the X-24A Flight Vehicle. Technical Report NASA TM X-1922, Research Engineering, NASA Dryden Flight Research Center.
Moes, Timothy R. and Whitmore, Stephen A. and Jordan Jr., Frank L. (1993) Flight and Wind-Tunnel Calibrations of a Flush Airdata Sensor at High Angles of Attack and Sideslip and at Supersonic Mach Numbers. Technical Report NASA TM-104265, Research Engineering, NASA Dryden Flight Research Center.
Garringer, Darwin J. and Saltzman, Edwin J. (1967) Flight Demonstration of a Skin-Friction Gage to a Local Mach Number of 4.9. Technical Report NASA Technical Note TN D-3830, Research Engineering, NASA Dryden Flight Research Center.
Saltzman, Edwin J. and Hintz, John (1967) Flight Evaluation of Splitter-Plate Effectiveness in Reducing Base Drag at Mach Numbers from 0.65 to 0.90. Technical Report NASA TM X-1376, Research Engineering, NASA Dryden Flight Research Center.
Matheny, Neil W. (1974) Flight Investigation of Approach and Flare From Simulated Breakout Altitude of a Subsonic Jet Transport and Comparison With Analytical Models. Technical Report NASA Technical Note TN D-7645, Research Engineering, NASA Dryden Flight Research Center.
Reed, Robert D. (1955) Flight Measurements of Horizontal-Tail Loads on the Bell X-5 Research Airplane at a Sweep Angle of 58.7 Degrees. Technical Report NACA RM H55E20a, Research Engineering, NASA Dryden Flight Research Center.
Knapp, Ronald J. and Johnson, Wallace E. (1953) Flight Measurements of Pressures on Base and Rear Part of Fuselage of the Bell X-1 Research Airplane at Transonic Speeds, Including Power Effects. Technical Report NACA RM-L52L01, Research Engineering, NASA Dryden Flight Research Center.
Carner, H. Arthur and Knapp, Ronald J. (1950) Flight Measurements of the Pressure Distribution on the Wing of the X-1 Airplane (10-Percent-Thick Wing) over a Chordwise Station near the Midspan, in Level Flight at Mach Numbers from 0.79 to 1.00 and in a Pull-Up at a Mach Number of 0.96. Technical Report NACA RM L50H04, Research Engineering, NASA Dryden Flight Research Center.
Johnson, Clinton T. (1955) Flight Measurements of the Vertical-Tail Loads on the Convair XF-92A Delta-Wing Airplane. Technical Report NACA RM H55H25, Research Engineering, NASA Dryden Flight Research Center.
Kuhl, Albert E. and Johnson, Clinton T. (1955) Flight Measurements of Wing Loads on the Convair XF-92A Delta-Wing Airplane. Technical Report NACA RM H55D12, Research Engineering, NASA Dryden Flight Research Center.
Mayer, John P. and Valentine, George M. (1951) Flight Measurements with the Douglas D-558-II (BuAero No. 37974) Research Airplane – Measurements of the Distribution of the Aerodynamic Load Among the Wing, Fuselage, and Horizontal Tail at Mach Numbers up to 0.87. Technical Report NACA RM L50J13, Research Engineering, NASA Dryden Flight Research Center.
Beeler, De E. and Bellman, Donald R. and Saltzman, Edwin J. (1956) Flight Techniques for Determining Airplane Drag at High Mach Numbers. Technical Report NACA TN 3821, Research Engineering, NASA Dryden Flight Research Center.
Gilyard, Glenn B. and Georgie, Jennifer and Barnicki, Joseph S. (1999) Flight Test of an Adaptive Configuration Optimization System for Transport Aircraft. Meeting Paper AIAA-1999-0831, Research Engineering, NASA Dryden Flight Research Center.
Zuniga, Fanny A. and Anderson, Bianca T. and Bertelrud, Arild (1992) Flight Test Results of Riblets at Supersonic Speeds. Technical Report NASA TM-4387, Research Engineering, NASA Dryden Flight Research Center.
Powers, Sheryll Goecke (1988) Flight Tests of External Modifications Used to Reduce Blunt Base Drag. Technical Report NASA TM-100433, Research Engineering, NASA Dryden Flight Research Center.
Powers, Sheryll Goecke and Webb, Lannie D. (1997) Flight Wing Surface Pressure and Boundary-Layer Data Report from the F-111 Smooth Variable-Camber Supercritical Mission Adaptive Wing. Technical Report NASA TM-4789, Research Engineering, NASA Dryden Flight Research Center.
Pyle, Jon S. and Steers, Louis L. (1975) Flight-Determined Lift and Drag Characteristics of an F-8 Airplane Modified with a Supercritical Wing with Comparisons to Wind-Tunnel Results. Technical Report NASA TM X-3250, Research Engineering, NASA Dryden Flight Research Center.
Horton, Victor W. and Eldredge, Richard C. and Klein, Richard E. (1965) Flight-Determined Low-Speed Lift and Drag Characteristics of the Lightweight M2-F1 Lifting Body. Technical Report NASA Technical Note TN D-3021, Research Engineering, NASA Dryden Flight Research Center.
Jordan, Gareth H. and Keener, Earl R. (1955) Flight-Determined Pressure Distributions Over a Section of the 35 Degree Swept Wing of the Douglas D-558-II Research Airplane at Mach Numbers up to 2.0. Technical Report NACA RM H55A03, Research Engineering, NASA Dryden Flight Research Center.
Saltzman, Edwin J. and Wang, K. Charles and Iliff, Kenneth W. (1999) Flight-Determined Subsonic Lift and Drag Characteristics of Seven Lifting-Body and Wing-Body Reentry Vehicle Configurations With Truncated Bases. Meeting Paper AIAA-1999-0383, Research Engineering, NASA Dryden Flight Research Center.
Fisher, David F. (1969) Flight-Measured Aerodynamic Drag of Two Large External Tanks Attached to the X-15-2 Airplane at Mach Numbers of 1.6 to 2.3. Technical Report NASA TM X-1895, Research Engineering, NASA Dryden Flight Research Center.
Steers, Louis L. (1979) Flight-Measured Afterbody Pressure Coefficients From an Airplane Having Twin Side-By-Side Jet Engines for Mach Numbers 0.6 to 1.6. Technical Report NASA TP-1549, Research Engineering, NASA Dryden Flight Research Center.
Monaghan, Richard C. (1978) Flight-Measured Buffet Characteristics of a Supercritical Wing and a Conventional Wing on a Variable-Sweep Airplane. Technical Report NASA TP-1244, Research Engineering, NASA Dryden Flight Research Center.
Quinn, Robert D. and Olinger, Frank V. (1969) Flight-Measured Heat Transfer and Skin Friction at a Mach Number of 5.25 and at Low Wall Temperatures. Technical Report NASA TM X-1921, Research Engineering, NASA Dryden Flight Research Center.
Powers, Sheryll Goecke (1978) Flight-Measured Pressure Characteristics of Aft-Facing Steps in High Reynolds Number Flow at Mach Numbers of 2.20, 2.50, and 2.80 and Comparison With Other Data. Technical Report NASA TM-72855, Research Engineering, NASA Dryden Flight Research Center.
Mizukami, Masashi and Jones, Daniel and Weinstock, Vladimir D. (2000) Flow Field Survey in the Test Region of the SR-71 Aircraft Test Bed Configuration. Technical Report NASA/TM-2000-209025, Research Engineering, NASA Dryden Flight Research Center.
Walsh, Kevin Robert (1985) Flow Field Survey Near the Rotational Plane of an Advanced Design Propeller on a JetStar Airplane. Technical Report NASA TM-86037, Research Engineering, NASA Dryden Flight Research Center.
Bjarke, Lisa J. (1991) Flow Visualization Study of a 1/48-Scale AFTI/F111 Model to Investigate Horizontal Tail Flow Disturbances. Technical Report NASA TM-101698, Research Engineering, NASA Dryden Flight Research Center.
Fisher, David F. and Meyer, Robert R. (1988) Flow Visualization Techniques for Flight Research. Technical Report NASA TM-100455, Research Engineering, NASA Dryden Flight Research Center.
McLain, L. J. and Palitz, Murray (1968) Flow-Field Investigations on the X-15 Airplane and Model up to Hypersonic Speeds. Technical Report NASA Technical Note TN D-4813, Research Engineering, NASA Dryden Flight Research Center.
Cotton, Lt. Stacey J. and Bjarke, Lisa J. (1994) Flow-Visualization Study of the X-29A Aircraft at High Angles of Attack Using a 1/48-Scale Model. Technical Report NASA TM-104268, Research Engineering, NASA Dryden Flight Research Center.
Fisher, David F. and Murri, Daniel G. (2001) Forebody Aerodynamics of the F-18 High Alpha Research Vehicle With Actuated Forebody Strakes. Meeting Paper MP-69-P-45, Research Engineering, NASA Dryden Flight Research Center.
Fisher, David F. and Murri, Daniel G. (1998) Forebody Flow Visualization on the F-18 HARV With Actuated Forebody Strakes. Technical Report NASA/TM-1998-206556, Research Engineering, NASA Dryden Flight Research Center.
Murray, James E. and Sim, Alex G. and Neufeld, David C. and Rennich, Patrick K. and Norris, Stephen R. and Hughes, Wesley S. (1994) Further Development and Flight Test of an Autonomous Precision Landing System Using a Parafoil. Technical Report NASA TM-4599, Research Engineering, NASA Dryden Flight Research Center.
Voracek, David F. and Reaves, Mercedes and Horta, Lucas G. and Potter, Starr (2002) Ground and Flight Test Structural Excitation Using Piezoelectric Actuators. Technical Report NASA TM-2002-210724, Research Engineering, NASA Dryden Flight Research Center.
Norris, Stephen R. and Haering Jr., Edward A. and Murray, James E. (1995) Ground-Based Sensors for the SR-71 Sonic Boom Propagation Experiment. Technical Report NASA TM-104310, Research Engineering, NASA Dryden Flight Research Center.
Curry, Robert E. and Bowers, Albion H. (1985) Ground-Effect Analysis of a Jet Transport Airplane. Technical Report NASA TM-85920, Research Engineering, NASA Dryden Flight Research Center.
Curry, Robert E. and Owens, Lewis R. (2003) Ground-Effect Characteristics of the Tu-144 Supersonic Transport Airplane. Technical Report NASA/TM-2003-212035, Research Engineering, NASA Dryden Flight Research Center.
Bahm, Catherine M. and Haering Jr., Edward A. (1995) Ground-Recorded Sonic Boom Signatures of F-18 Aircraft in Formation Flight. Technical Report NASA TM-104312, Research Engineering, NASA Dryden Flight Research Center.
Ayers, Theodore G. and Hallissy, James B. (1981) Historical Background and Design Evolution of the Transonic Aircraft Technology Supercritical Wing. Technical Report NASA TM-81356, Research Engineering, NASA Dryden Flight Research Center.
Lind, Rick and Prazenica, Richard J. and Brenner, Martin J. and Baldelli, Dario H. (2004) Identifying Parameter-Dependent Volterra Kernels to Predict Aeroelastic Instabilities. Conference Paper AIAA-2004-1517, Research Engineering, NASA Dryden Flight Research Center.
Curry, Robert E. and Mendenhall, Michael R. and Moulton, Bryan (1992) In-Flight Evaluation of Aerodynamic Predictions of an Air-Launched Space Booster. Technical Report NASA TM-104246, Research Engineering, NASA Dryden Flight Research Center.
Fisher, David F. and Del Frate, John H. and Richwine, David M. (1990) In-Flight Flow Visualization Characteristics of the NASA F-18 High Alpha Research Vehicle at High Angles of Attack. Technical Report NASA TM-4193, Research Engineering, NASA Dryden Flight Research Center.
Del Frate, John H. and Saltzman, John A. (1992) In-Flight Flow Visualization Results From the X-29A Aircraft at High Angles of Attack. Technical Report NASA TM-4430, Research Engineering, NASA Dryden Flight Research Center.
Del Frate, John H. and Fisher, David F. and Zuniga, Fanny A. (1990) In-Flight Flow Visualization with Pressure Measurements at Low Speeds on the NASA F-18 High Alpha Research Vehicle. Technical Report NASA TM-101726, Research Engineering, NASA Dryden Flight Research Center.
Wang, Kon-Sheng Charles (1994) In-Flight Imaging of Transverse Gas Jets Injected Into Transonic and Supersonic Crossflows: Design and Development. Technical Report NASA CR-186031, 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.
Saltzman, Edwin J. and Wang, K. Charles and Iliff, Kenneth W. (2007) In-Flight Subsonic Lift and Drag Characteristics Unique to Blunt-Based Lifting Reentry Vehicles. Journal Article AIAA-18365, Research and Engineering, NASA Dryden Flight Research Center. Journal of Spacecraft and Rockets 44(2):299-309.
Meyer Jr., Robert R. and Jennett, Lisa A. (1985) In-Flight Surface Oil-Flow Photographs With Comparisons to Pressure Distribution and Boundary-Layer Data. Technical Report NASA TP-2395, 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.
Gilyard, Glenn (1997) In-Flight Transport Performance Optimization: An Experimental Flight Research Program and an Operational Scenario. Technical Report NASA/TM-97-206229, Research Engineering, NASA Dryden Flight Research Center.
Davis, Mark C. and Saltzman, John A. (2000) In-Flight Wing Pressure Distributions for the NASA F/A-18A High Alpha Research Vehicle. Technical Report NASA/TP-2000-209018, Research Engineering, NASA Dryden Flight Research Center.
Hansen, Jennifer L. and Cobleigh, Brent R. (2002) Induced Moment Effects of Formation Flight Using Two F/A-18 Aircraft. Technical Report NASA/TM-2002-210732, Research Engineering, NASA Dryden Flight Research Center.
Haering Jr., Edward A. and Cliatt II, Larry J. and Bunce, Thomas J. and Gabrielson, Thomas B. and Sparrow, Victor W. and Locey, Lance L. (2008) Initial Results from the Variable Intensity Sonic Boom Propagation Database. Conference Presentation AIAA-2008-3034, Research and Engineering, NASA Dryden Flight Research Center.
Authors, Various (1982) KC-135 Winglet Program Review. Technical Report NASA Conference Publication CP-2211, Research Engineering, NASA Dryden Flight Research Center.
Vachon, Michael Jacob and Moes, Timothy R. and Corda, Stephen (2005) Local Flow Conditions for Propulsion Experiments on the NASA F-15B Propulsion Flight Test Fixture. Technical Report NASA/TM-2005-213670, Research Engineering, NASA Dryden Flight Research Center.
Cox, Timothy H. and Marshall, Alisa (2000) Longitudinal Handling Qualities of the Tu-144LL Airplane and Comparisons With Other Large, Supersonic Aircraft. Technical Report NASA/TM-2000-209020, Research Engineering, NASA Dryden Flight Research Center.
Webb, Lannie D. (1985) Mach Number and Flow-Field Calibration at the Advanced Design Propeller Location on the JetStar Airplane. Technical Report NASA TM-84923, Research Engineering, NASA Dryden Flight Research Center.
Whitmore, Stephen A. and Moes, Timothy R. (1994) Measurement Uncertainty and Feasibility Study of a Flush Airdata System for a Hypersonic Flight Experiment. Technical Report NASA TM-4627, Research Engineering, NASA Dryden Flight Research Center.
Green, Karen S. and Putnam, Terrill W. (1974) Measurements of Sonic Booms Generated by an Airplane Flying at Mach 3.5 and 4.8. Technical Report NASA TM X-3126, Research Engineering, NASA Dryden Flight Research Center.
Beeler, De E. and McLaughlin, Milton D. and Clift, Dorothy C. (1948) Measurements of the Chordwise Pressure Distributions Over the Wing of the XS-1 Research Airplane in Flight. Technical Report NACA RM L8G21, Research Engineering, NASA Dryden Flight Research Center.
Bowers, Albion H. and Noffz, Gregory K. and Grafton, Sue B. and Mason, Mary L. and Peron, Lee R. (1991) Multiaxis Thrust Vectoring Using Axisymmetric Nozzles and Postexit Vanes on an F/A-18 Configuration Vehicle. Technical Report NASA TM-101741, 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.
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.
Gilyard, Glenn B. and Bolonkin, Alexander (2000) Optimal Pitch Thrust-Vector Angle and Benefits for all Flight Regimes. Technical Report NASA/TM-2000-209021, Research Engineering, NASA Dryden Flight Research Center.
Anderson, Bianca T. and Bohn-Meyer, Marta (1992) Overview of Supersonic Laminar Flow Control Research on the F-16XL Ships 1 and 2. Technical Report NASA TM-104257, Research Engineering, NASA Dryden Flight Research Center.
Budd, Gerald D. (1987) Predicted Pitching Moment Characteristics of X-29A Aircraft. Technical Report NASA TM-88284, Research Engineering, NASA Dryden Flight Research Center.
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.
Jordan, Gareth H. and Hutchins Jr., C. Kenneth (1955) Preliminary Flight-Determined Pressure Distributions Over the Wing of the Douglas X-3 Research Airplane at Subsonic and Transonic Mach Numbers. Technical Report NACA RM H55A10, Research Engineering, NASA Dryden Flight Research Center.
Drake, Hubert M. and Goodman, Harold R. and Hoover, Herbert H. (1948) Preliminary Results of NACA Transonic Flights of the XS-1 Airplane with 10-Percent-Thick Wing and 8-Percent-Thick Horizontal Tail. Technical Report NACA RM L8I29, Research Engineering, NASA Dryden Flight Research Center.
Saltzman, Edwin J. and Del Frate, John H. and Sabsay, Catherine M. and Yarger, Jill M. (1992) Pressure Distribution for the Wing of the YAV-8B Airplane; With and Without Pylons. Technical Report NASA TM-4429, Research Engineering, NASA Dryden Flight Research Center.
Johnson, Steven and Murphy, Kelly (1994) Pressure-Sensing Performance of Upright Cylinders in a Mach 10 Boundary-Layer. Technical Report NASA TM-4633, 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.
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 I. Technical Report NASA Conference Publication CP-3256, Volume I, Research Engineering, NASA Dryden Flight Research Center.
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.
Mangalam, Arun S. and Moes, Timothy R. (2004) Real-Time Unsteady Loads Measurements Using Hot-Film Sensors. Technical Report NASA/TM-2004-212854, Research Engineering, NASA Dryden Flight Research Center.
Mangalam, Arun S. and Moes, Timothy R. (2004) Real-Time Unsteady Loads Measurements Using Hot-Film Sensors. Meeting Paper AIAA-2004-5371, Research Engineering, NASA Dryden Flight Research Center.
Thornton, Stephen V. (1993) Reduction of Structural Loads Using Maneuver Load Control on the Advanced Fighter Technology Integration (AFTI)/F-111 Mission Adaptive Wing. Technical Report NASA TM-4526, Research Engineering, NASA Dryden Flight Research Center.
McLaughlin, Milton D. and Clift, Dorothy C. (1948) Results Obtained During a Dive Recovery of the Bell XS-1 Airplane to High Lift Coefficients at a Mach Number Greater than 1.0. Technical Report NACA RM L8C23a, Research Engineering, NASA Dryden Flight Research Center.
Drake, Hubert M. and McLaughlin, Milton D. and Goodman, Harold R. (1948) Results Obtained During Accelerated Transonic Tests of the Bell XS-1 Airplane in Flights to a Mach Number of 0.92. Technical Report NACA RM L8A05a, Research Engineering, NASA Dryden Flight Research Center.
Goodman, Harold R. and Drake, Hubert M. (1948) Results Obtained During Extension of U.S. Air Force Transonic-Flight Tests of XS-1 Airplane. Technical Report NACA RM L8I28, Research Engineering, NASA Dryden Flight Research Center.
Sim, Alex G. (1973) Results of a Feasibility Study Using the Newton-Raphson Digital Computer Program to Identify Lifting Body Derivatives from Flight Data. Technical Report NASA TM X-56017, Research Engineering, NASA Dryden Flight Research Center.
Williams, W. C. and Beeler, De E. (1948) Results of Preliminary Flight Tests of the XS-1 Airplane (8-Percent Wing) to a Mach Number of 1.25. Technical Report NACA RM L8A23a, Research Engineering, NASA Dryden Flight Research Center.
Fisher, David F. and Cobleigh, Brent R. and Banks, Daniel W. and Hall, Robert M. and Wahls, Richard W. (1998) Reynolds Number Effects at High Angles of Attack. Technical Report NASA/TP-1998-206553, 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.
Banner, Richard D. and Malvestuto Jr., Frank S. (1956) Skin and Structural Temperature Measurements on Research Airplanes at Supersonic Speeds. Technical Report NACA-CONF-26-Oct-56-p101-112, 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.
Hanson, Curtis E. (2009) Static Aeroelastic Effects of Formation Flight for Slender Unswept Wings. Technical Report NASA/TM-2009-214649, Research and Engineering, NASA Dryden Flight Research Center.
Fisher, David F. and Del Frate, John H. and Zuniga, Fanny A. (1991) Summary of In-Flight Flow Visualization Obtained From the NASA High Alpha Research Vehicle. Technical Report NASA TM-101734, Research Engineering, NASA Dryden Flight Research Center.
Marshall, Laurie A. (2000) Summary of Transition Results from the F-16XL-2 Supersonic Laminar Flow Control Experiment. Meeting Paper AIAA-2000-4418, Research Engineering, NASA Dryden Flight Research Center.
Fisher, David F. and Richwine, David M. and Banks, Daniel W. (1988) Surface Flow Visualization of Separated Flows on the Forebody of an F-18 Aircraft and Wind-Tunnel Model. Technical Report NASA TM-100436, Research Engineering, NASA Dryden Flight Research Center.
Keener, Earl R. and Pierce, Mary (1950) Tabulated Pressure Coefficients and Aerodynamic Characteristics Measured in Flight on the Wing of the Douglas D-558-I Airplane for a 1g Stall, a Speed Run to a Mach Number of 0.90, and a Wind-Up Turn at a Mach Number of 0.86. Technical Report NACA RM L50J10, Research Engineering, NASA Dryden Flight Research Center.
Keener, Earl R. and Peele, James R. and Woodbridge, Julia B. (1951) Tabulated Pressure Coefficients and Aerodynamic Characteristics Measured in Flight on the Wing of the Douglas D-558-I Airplane Throughout the Normal-Force-Coefficient Range at Mach Numbers of 0.67, 0.74, 0.78, and 0.82. Technical Report NACA RM L50L12a, Research Engineering, NASA Dryden Flight Research Center.
Carner, H. Arthur and Payne, Mary M. (1950) Tabulated Pressure Coefficients and Aerodynamic Characteristics Measured on the Wing of the Bell X-1 Airplane in Level Flight at Mach Numbers from 0.79 to 1.00 and in a Pull-Up at a Mach Number of 0.96. Technical Report NACA RM L50H25, 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.
Banks, Daniel W. and Fisher, David F. and Hall, Robert M. and Erickson, Gary E. and Murri, Daniel G. and Grafton, Sue B. and Sewall, William G. (1997) The F/A-18 High-Angle-of-Attack Ground-to-Flight Correlation: Lessons Learned. Technical Report NASA TM-4783, Research Engineering, NASA Dryden Flight Research Center.
Banks, Daniel W. and Fisher, David F. and Hall, Robert M. and Erickson, Gary E. and Murri, Daniel G. and Grafton, Sue B. and Sewall, William G. (1996) The F/A-18 High-Angle-of-Attack Ground-to-Flight Correlation: Lessons Learned. In Proceedings High-Angle-of-Attack Technology Conference, pages 91-129, NASA Langley Research Center, Hampton, Virginia.
Hansen, Jennifer L. and Murray, James E. and Campos, Norma V. (2005) The NASA Dryden Flight Test Approach to an Aerial Refueling System. Technical Report NASA/TM-2005-212859, 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.
Curry, Robert E. and Meyer Jr., Robert R. and O'Connor, Maureen (1984) The Use of Oil for In-Flight Flow Visualization. Technical Report NASA TM-84915, 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.
Balakrishnan, A. V. (1999) Unsteady Aerodynamics – Subsonic Compressible Inviscid Case. Technical Report NASA/CR-1999-206583, Research Engineering, NASA Dryden Flight Research Center.
Curry, Robert E. (1978) Utilization of the Wing-Body Aerodynamic Analysis Program. Technical Report NASA TM-72856, Research Engineering, NASA Dryden Flight Research Center.
Beeler, De E. and Gerard, George (1947) Wake Measurements Behind a Wing Section of a Fighter Airplane in Fast Dives. Technical Report NACA TN-1190, Research Engineering, NASA Dryden Flight Research Center.
Cobleigh, Brent R. and Del Frate, John (1994) Water Tunnel Flow Visualization Study of a 4.4% Scale X-31 Forebody. Technical Report NASA TM-104276, Research Engineering, NASA Dryden Flight Research Center.
Johnson, Steven A. and Fisher, David F. (1990) Water-Tunnel Study Results of a TF/A-18 and F/A-18 Canopy Flow Visualization. Technical Report NASA TM-101705, Research Engineering, NASA Dryden Flight Research Center.
Davis, Mark C. and Sim, Alexander G. and Rhode, Matthew and Johnson, Kevin D. (2006) Wind Tunnel Results of the B-52B with the X-43A Stack. Conference Paper AIAA-2006-3850.
Moes, Timothy R. and Cobleigh, Brent R. and Connors, Timothy R. and Cox, Timothy H. and Smith, Stephen C. and Shirakata, Norm (1996) Wind-Tunnel Development of an SR-71 Aerospike Rocket Flight Test Configuration. Technical Report NASA TM-4749, Research Engineering, NASA Dryden Flight Research Center.
Montoya, Earl J. and Nugent, Jack (1969) Wind-Tunnel Force and Pressure Tests of Rocket-Engine Nozzle Extensions on the 0.0667-Scale X-15-2 Model at Supersonic and Hypersonic Speeds. Technical Report NASA TM X-1759, Research Engineering, NASA Dryden Flight Research Center.
Arnaiz, Henry H. and Peterson Jr., John B. and Daugherty, James C. (1980) Wind-Tunnel/Flight Correlation Study of Aerodynamic Characteristics of a Large Flexible Supersonic Cruise Airplane (XB-70-1). III - A Comparison Between Characteristics Predicted From Wind-Tunnel Measurements and Those Measured In Flight. Technical Report NASA TP-1516, Research Engineering, NASA Dryden Flight Research Center.
Keener, Earl R. and Jordan, Gareth H. (1956) Wing Loads and Load Distributions Throughout the Lift Range of the Douglas X-3 Research Airplane at Transonic Speeds. Technical Report NASA RM H56G13, Research Engineering, NASA Dryden Flight Research Center.
Keener, Earl R. and Jordan, Gareth H. (1955) Wing Pressure Distributions Over the Lift Range of the Convair XF-92A Delta-Wing Airplane at Subsonic and Transonic Speeds. Technical Report NACA RM H55G07, Research Engineering, NASA Dryden Flight Research Center.
Banner, Richard D. and Reed, Robert D. and Marcy, William L. (1955) Wing-Load Measurements of the Bell X-5 Research Airplane at a Sweep Angle of 58.7 Degrees. Technical Report NACA RM H55A11, Research Engineering, NASA Dryden Flight Research Center.
Clarke, Robert and Burken, John J. and Bosworth, John T. and Bauer, Jeffrey E. (1996) X-29 flight control system: lessons learned, in Advances in Aircraft Flight Control, chapter 13, pages 345-367. Taylor & Francis.
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.
Clarke, Robert and Burken, John J. and Bosworth, John T. and Bauer, Jeffrey E. (1995) X-29 Flight Control System: Lessons Learned. Conference Presentation AGARD-CP-560, Paper No. 12, Research Engineering, NASA Dryden Flight Research Center.
This list was generated on Sun Nov 22 18:15:16 PST 2009.
