Subject: X-15
Number of records: 72.
Iliff, Kenneth W. and Shafer, Mary F. (1993) A Comparison of Hypersonic Flight and Prediction Results. Meeting Paper AIAA-1993-0311, Research Engineering, NASA Dryden Flight Research Center.
Iliff, Kenneth W. and Shafer, Mary F. (1995) A Comparison of Hypersonic Vehicle Flight and Prediction Results. Technical Report NASA TM-104313, Research Engineering, NASA Dryden Flight Research Center.
Taylor Jr., Lawrence W. and Iliff, Kenneth W. and Powers, Bruce G. (1969) A Comparison of Newton-Raphson and Other Methods for Determining Stability Derivatives from Flight Data. Conference Paper AIAA-1969-315, Research Engineering, NASA Flight Research Center.
Quinn, Robert D. and Gong, Leslie (2000) A Method for Calculating Transient Surface Temperatures and Surface Heating Rates for High-Speed Aircraft. Technical Report NASA/TP-2000-209034, Research Engineering, NASA Dryden Flight Research Center.
Rediess, Herman A. and Whitaker, H. Philip (1969) A New Model Performance Index for the Engineering Design of Flight Control Systems. Conference Paper AIAA-1969-885, Research Engineering, NASA 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.
Larson, Terry J. and Covington, M. Alan (1966) A Technique for Measuring Mesospheric Densities with the X-15 Research Airplane. Meeting Paper AIAA-1966-441, Research Engineering, NASA Flight Research Center.
Bogue, Rodney K. and Webb, Lannie D. (1968) Advanced Air Data Sensing Techniques. Technical Report NASA TM X-61115, 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.
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.
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.
Thompson, Milton O. and Weil, Joseph and Holleman, Euclid C. (1967) An Assessment of Lifting Reentry Flight Control Requirements During Abort, Terminal Glide, and Approach and Landing Situations. Technical Report NASA TM X-59119, 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.
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.
Carpenter, Richard (1970) Biotechnology Problems Relative to the Space Shuttle Vehicle, Meeting Paper AIAA-1970-1327, Research Engineering, NASA Flight Research Center.
Lewis, Thomas L. and Banner, Richard D. (1971) Boundary-Layer Transition Detection on The X-15 Vertical Fin Using Surface-Pressure-Fluctuation Measurements. Technical Report NASA TM X-2466, 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.
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.
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.
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.
Holleman, Euclid C. and Adkins, Elmor J. (1964) Contributions of the X-15 Program to Lifting Entry Technology. Meeting Paper AIAA-1964-17, Research Engineering, NASA Flight Research Center.
Day, Richard E. (1997) Coupling Dynamics in Aircraft: A Historical Perspective. NASA Special Publication SP-532, Research Engineering, NASA Dryden Flight Research Center. National Aeronautics and Space Administration.
Carpenter, Richard and Roman, James (1971) Digital Automatic Data Reduction Techniques Used in a 1000-Flight Biomedical Study. Technical Report NASA Technical Note TN D-6601, 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.
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.
By Staff of the, Flight Research Center (1971) Experience With the X-15 Adaptive Flight Control System. Technical Report NASA Technical Note TN D-6208, 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.
Monaghan, Richard C. and Fields, Roger A. (1973) Experiments to Study Strain-Gage Load Calibrations on a Wing Structure at Elevated Temperatures. Technical Report NASA Technical Note TN D-7390, 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.
Cary, John P. and Keener, Earl R. (1965) Flight Evaluation of the X-15 Ball-Nose Flow-Direction Sensor as an Air-Data System. Technical Report NASA Technical Note TN D-2923, 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.
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.
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.
Fields, Roger A. (1992) Flight Vehicle Thermal Testing With Infrared Lamps. Technical Report NASA TM-4336, Research Engineering, NASA Dryden Flight Research Center.
Fischel, Jack and Webb, Lannie D. (1964) Flight-Informational Sensors, Display, and Space Control of the X-15 Airplane for Atmospheric and Near-Space Flight Missions. Technical Report NASA Technical Note TN D-2407, 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.
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.
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.
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.
Dryden, Dr. Hugh L. (1956) General Background of the X-15 Research-Airplane Project. Technical Report NACA-CONF-26-Oct-56-pxvii-xxi, Research Engineering, NASA Dryden Flight Research Center.
Painter, Weneth D. and Sitterle, George J. (1972) Ground and Flight Test Methods For Determining Limit Cycle and Structural Resonance Characteristics of Aircraft Stability Augmentation Systems. Technical Report NASA Technical Note TN D-6867, 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.
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.
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.
Taback, I. and Truszynski, G. M. (1956) Instrumentation for the X-15. Technical Report NACA-CONF-26-Oct-56-p183-191, Research Engineering, NASA Dryden Flight Research Center.
Burcham Jr., Frank W. and Nugent, Jack (1970) Local Flow Field Around a Pylon-Mounted Dummy Ramjet Engine on the X-15-2 Airplane for Mach Numbers from 2.0 to 6.7. Technical Report NASA Technical Note TN D-5638, Research Engineering, NASA Dryden Flight Research Center.
Palitz, Murray (1966) Measured and Calculated Flow Conditions on the Forward Fuselage of the X-15 Airplane and Model at Mach Numbers from 3.0 to 8.0. Technical Report NASA Technical Note TN D-3447, 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.
Wolowicz, Chester H. and Gossett, Terrence D. (1965) Operational and Performance Characteristics of the X-15 Spherical, Hypersonic Flow-Direction Sensor. Technical Report NASA Technical Note TN D-3070, 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.
Row, Perry V. and Fischel, Jack (1963) Operational Flight-Test Experience with the X-15 Airplane. Conference Paper AIAA-1963-075, Research Engineering, NASA 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.
Holleman, Euclid C. (1964) Piloting Performance During the Boost of the X-15 Airplane to High Altitude. Technical Report NASA Technical Note TN D-2289, 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.
(1991) Proceedings of the X-15 First Flight 30th Anniversary Celebration. Conference Proceedings Report NASA CP-3105, X-15 First Flight 30th Anniversary Celebration, Edwards, California.
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.
Jones, Daniel S. and Ray, Ronald J. and Phillips, Paul (2005) Rehabilitation of the Rocket Vehicle Integration Test Stand at Edwards Air Force Base. Technical Report NASA/TM-2005-212863, Research Engineering, NASA Dryden Flight Research Center.
Saltzman, Edwin J. and Ayers, Theodore G. (1995) Selected Examples of NACA/NASA Supersonic Flight Research. Technical Report NASA Special Publication SP-513, Research Engineering, NASA Dryden Flight Research Center. National Aeronautics and Space Administration.
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.
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.
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.
Montoya, Earl J. and Larson, Terry J. (1964) Stratosphere and Mesosphere Density-Height Profiles Obtained with the X-15 Airplane. Technical Report NASA TM X-56009, Research Engineering, NASA Dryden Flight Research Center.
Stillwell, Wendell H. (1956) Studies of Reaction Controls. Technical Report NACA-CONF-26-Oct-56-p175-181, 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.
Dana, William H. (1993) The X-15 Airplane - Lessons Learned. Meeting Paper AIAA-1993-0309, 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.
Noll, Richard B. and Halasey, Robert L. (1963) Theoretical Investigation of the Slideout Dynamics of a Vehicle Equipped with a Tricycle Skid-Type Landing-Gear System. Technical Report NASA Technical Note TN D-1828, Research Engineering, NASA Dryden Flight Research Center.
Burcham Jr., Frank W. (1968) Wind-Tunnel Calibration of a 40 Degree Conical Pressure Probe at Mach Numbers from 3.5 to 7.4. Technical Report NASA Technical Note TN D-4678, 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.
Stillwell, Wendell H. (1965) X-15 Research Results With a Selected Bibliography. National Aeronautics and Space Administration.
This list was generated on Fri Oct 10 18:17:11 PDT 2008.
