Subject: YF-12
Number of records: 40.
DeMarco, Diane M. (1974) A Dynamic Pressure Generator for Checking Complete Pressure Sensing Systems Installed on an Airplane. Technical Report NASA TM X-56026, 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.
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.
Gilyard, Glenn B. and Berry, Donald T. and Belte, Daumants (1972) Analysis of a Lateral-Directional Airframe/Propulsion System Interaction of a Mach 3 Cruise Aircraft. Meeting Paper AIAA-1972-961, Research Engineering, NASA Dryden Flight Research Center.
Redin, Paul C. (1981) Application of a Performance Modeling Technique to an Airplane with Variable Sweep Wings. Technical Report NASA TP-1855, Research Engineering, NASA Dryden Flight Research Center.
Brilliant, Capt. Howard M. and Bauer, Carol A. (1977) Comparison of Estimated with Measured Maximum Instantaneous Distortion Using Flight Data from an Axisymmetric Mixed Compression Inlet. Meeting Paper AIAA-1977-876, 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.
Gilyard, Glenn B. and Burken, John J. (1980) Development and Flight Test Results of an Autothrottle Control System at Mach 3 Cruise. Technical Report NASA TP-1621, Research Engineering, NASA Dryden Flight Research Center.
Webb, William L. and Reukauf, Paul J. (1973) Development of a Turbine Inlet Gas Temperature Measurement and Control System Using a Fluidic Temperature Sensor. Meeting Paper AIAA-1973-1251, Research Engineering, NASA Dryden Flight Research Center.
Stoll, Frederick and Tremback, Jeffrey W. and Arnaiz, Henry H. (1979) Effect of Number of Probes and Their Orientation on the Calculation of Several Compressor Face Distortion Descriptors. Technical Report NASA TM-72859, Research Engineering, NASA Dryden Flight Research Center.
Schweikhard, W.G. and Gilyard, G.B. and Talbot, J.E. and Brown, T.W. (1976) Effects of Atmospheric Conditions on the Operating Characteristics of Supersonic Cruise Aircraft. IAF Paper 76-112, Research Engineering, NASA Dryden Flight Research Center.
Cox, Timothy H. and Jackson, Dante W. (1997) Evaluation of High-Speed Civil Transport Handling Qualities Criteria With Supersonic Flight Data. Technical Report NASA TM-4791, Research Engineering, NASA Dryden Flight Research Center.
Gilyard, Glenn B. and Smith, John W. and Falkner, Victor L. (1974) Flight Evaluation of a Mach 3 Cruise Longitudinal Autopilot. Meeting Paper AIAA-1974-910, Research Engineering, NASA Dryden Flight Research Center.
Love, James E. and Fox, William J. and Wicklund, Edward J. (1974) Flight Study of a Vehicle Operational Status and Monitoring System. Technical Report NASA Technical Note TN D-7546, 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.
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.
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.
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.
Reukauf, Paul J. and Schweikhard, William G. and Arnaiz, Henry (1974) Flight-Test Techniques for Obtaining Valid Comparisons of Wind-Tunnel and Flight Results from Tests on a YF-12 Mixed-Compression Inlet. Meeting Paper AIAA-1974-1195, Research Engineering, NASA Dryden Flight Research Center.
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.
Ehernberger, L. J. (1987) High Altitude Turbulence for Supersonic Cruise Vehicles. Technical Report NASA TM-88285, Research Engineering, NASA Dryden Flight Research Center.
Quinn, Robert D. and Gong, Leslie (1980) In-Flight Boundary-Layer Measurements on a Hollow Cylinder at a Mach Number of 3.0. Technical Report NASA TP-1764, Research Engineering, NASA Dryden Flight Research Center.
Johnson, Harold J. and Montoya, Earl J. (1973) Local Flow Measurements at The Inlet Spike Tip of a Mach 3 Supersonic Cruise Airplane. Technical Report NASA Technical Note TN D-6987, 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.
Powers, Bruce G. (1977) Phugoid Charcteristics of a YF-12 Airplane with Variable-Geometry Inlets Obtained in Flight Tests at a Mach Number of 2.9. Technical Report NASA TP-1107, Research Engineering, NASA Dryden Flight Research Center.
Burcham Jr., Frank W. and Holzman, Jon K. and Reukauf, Paul J. (1973) Preliminary Results of Flight Tests of the Propulsion System of the YF-12 Airplane at Mach Numbers to 3.0. Meeting Paper AIAA-1973-1314, 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.
Gilyard, Glenn B. and Smith, John W. (1978) Results From Flight and Simulator Studies of a Mach 3 Cruise Longitudinal Autopilot. Technical Report NASA TP-1180, Research Engineering, NASA Dryden Flight Research Center.
Wilson, Ronald J. and Cazier Jr., Frank W. and Larson, Richard R. (1973) Results of Ground Vibration Tests on a YF-12 Airplane. Technical Report NASA TM X-2880, Research Engineering, NASA Dryden Flight Research Center.
Kordes, E.E. and Curtis, A.R. (1975) Results of NASTRAN Modal Analyses and Ground Vibration Tests on the YF-12A Airplane. Meeting Paper ASME Paper 75/WA/Aero-8, 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 and Engineering, NASA Dryden Flight Research Center.
Reukauf, Paul J. and Burcham Jr., Frank W. and Holzman, Jon K. (1975) Status of a Digital Integrated Propulsion/Flight Control System for the YF-12 Airplane. Conference Paper AIAA-1975-1180, Research Engineering, NASA Dryden Flight Research Center.
Albers, James A. (1976) Status of the NASA YF-12 Propulsion Research Program. Technical Report NASA TM X-56039, Research Engineering, NASA Dryden Flight Research Center.
Cox, Timothy H. and Jackson, Dante (1997) Supersonic Flying Qualities Experience Using the SR-71. Meeting Paper AIAA-1997-3654, Research Engineering, NASA Dryden Flight Research Center.
Bangert, L.H. and Burcham Jr., F.W. and Mackall, K.G. (1980) YF-12 Inlet Supression of Compressor Noise: First Results. Meeting Paper AIAA-1980-0099, Research Engineering, NASA Dryden Flight Research Center.
This list was generated on Mon Nov 23 18:17:36 PST 2009.
