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Subject: XB-70


Number of records: 50.

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.

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.

Whitmore, Stephen A. and Hurtado, Marco and Rivera, Jose and Naughton, Jonathan W. (2000) A Real-Time Method for Estimating Viscous Forebody Drag Coefficients. Technical Report NASA/TM-2000-209015, Research Engineering, NASA Dryden Flight Research Center.

Powers, Bruce G. (1968) A Review of Transport Handling-Qualities Criteria in Terms of Preliminary XB-70 Flight Experience. Technical Report NASA TM X-1584, 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.

Wolowicz, Chester H. (1966) Analysis of an Emergency Deceleration and Descent of the XB-70-1 Airplane due to Engine Damage Resulting from Structural Failure. Technical Report NASA TM X-1195, Research Engineering, NASA Dryden Flight Research Center.

Saltzman, Edwin J. and Goecke, Sheryll A. and Pembo, Chris (1968) Base Pressure Measurements on the XB-70 Airplane at Mach Numbers from 0.4 to 3.0. Technical Report NASA TM X-1612, Research Engineering, NASA Dryden Flight Research Center.

Wolowicz, Chester H. and Yancey, Roxanah B. (1973) Comparison of Predictions of the XB-70-1 Longitudinal Stability and Control Derivatives With Flight Results For Six Flight Conditions. Technical Report NASA TM X-2881, Research Engineering, NASA Dryden Flight Research Center.

Iliff, Kenneth W. and Taylor Jr., Lawrence W. (1972) Determination of Stability Derivatives from Flight Data Using a Newton-Raphson Minimization Technique. Technical Report NASA Technical Note TN D-6579, Research Engineering, NASA Dryden Flight Research Center.

Martin, Richard A. (1970) Dynamic Analysis of XB-70-1 Inlet Pressure Fluctuations During Takeoff and Prior to a Compressor Stall at Mach 2.5. Technical Report NASA Technical Note TN D-5826, 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.

Wilson, Ronald J. and Love, Betty J. and Larson, Richard R. (1971) Evaluation of Effects of High-Altitude Turbulence Encounters on the XB-70 Airplane. Technical Report NASA Technical Note TN D-6457, 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.

Webb, Lannie D. and Washington, Harold P. (1972) Flight Calibration of Compensated and Uncompensated Pitot-Static Airspeed Probes and Application of the Probes to Supersonic Cruise Vehicles. Technical Report NASA Technical Note TN D-6827, Research Engineering, NASA Dryden Flight Research Center.

Lock, Wilton P. and Kordes, Eldon E. and McKay, James M. and Wykes, John H. (1973) Flight Investigation of a Structural Mode Control System for the XB-70 Aircraft. Technical Report NASA Technical Note TN D-7420, Research Engineering, NASA Dryden Flight Research Center.

McKay, James M. and Kordes, Eldon E. and Wykes, John H. (1973) Flight Investigation of XB-70 Structural Response to Oscillatory Aerodynamic Shaker Excitation and Correlation with Analytical Results. Technical Report NASA Technical Note TN D-7227, 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.

Arnaiz, Henry H. (1977) Flight-Measured Lift and Drag Characteristics of a Large, Flexible, High Supersonic Cruise Airplane. Technical Report NASA TM X-3532, 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.

Berry, Donald T. and Powers, Bruce G. (1970) Flying Qualities of a Large, Supersonic Aircraft in Cruise and Landing Approach, Conference Paper AIAA-1970-566, Research Engineering, NASA Flight Research Center.

Berry, Donald T. and Powers, Bruce G. (1970) Handling Qualities of the XB-70 Airplane in the Landing Approach. Technical Report NASA Technical Note TN D-5676, 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.

Maglieri, Domenic J. and Sothcott, Victor E. and Hicks, John (1990) Influence of Vehicle Configuration and Flight Profile on X-30 Sonic Booms. Meeting Paper AIAA-1990-5224 Research Engineering, NASA Dryden Flight Research Center.

Gallagher, Robert J. (1970) Investigation of a Digital Simulation of the XB-70 Inlet and its Application to Flight-Experienced Free-Stream Disturbances at Mach Numbers of 2.4 to 2.6. Technical Report NASA Technical Note TN D-5827, Research Engineering, NASA Dryden Flight Research Center.

Wilson, Ronald J. and McKay, James M. (1968) Landing Loads and Accelerations of the XB-70-1 Airplane. Technical Report NASA Technical Note TN D-4836, Research Engineering, NASA Dryden Flight Research Center.

Fulton Jr., Fitzhugh L. (1968) Lessons from the XB-70 as Applied to the Supersonic Transport. Technical Report NASA TM X-56014, 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.

Beaulieu, Warren and Campbell, Ralph and Burcham, William (1968) Measurement of XB-70 Propulsion Performance Incorporating the Gas Generator Method. Conference Paper AIAA-1968-594, Research Engineering, NASA Flight Research Center.

Lewis, Thomas L. and Dods Jr., Jules B. and Hanly, Richard D. (1973) Measurements of Surface-Pressure Fluctuations on the XB-70 Airplane at Local Mach Numbers up to 2.45. Technical Report NASA Technical Note TN D-7226, Research Engineering, NASA Dryden Flight Research Center.

Ehernberger, L. J. (1968) Meteorological Aspects of High-Altitude Turbulence Encountered by the XB-70 Airplane. Technical Report NASA TM X-61114, Research Engineering, NASA Dryden Flight Research Center.

Szalai, Kenneth J. (1971) Motion Cue and Simulation Fidelity Aspects of the Validation of a General Purpose Airborne Simulator. Technical Report NASA Technical Note TN D-6432, 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.

Kordes, Eldon E. and Love, Betty J. (1967) Preliminary Evaluation of XB-70 Airplane Encounters with High-Altitude Turbulence. Technical Report NASA Technical Note TN D-4209, Research Engineering, NASA Dryden Flight Research Center.

Wolowicz, Chester H. and Strutz, Larry W. and Gilyard, Glenn B. and Matheny, Neil W. (1968) Preliminary Flight Evaluation of the Stability and Control Derivatives and Dynamic Characteristics of the Unaugmented XB-70-1 Airplane Including Comparisons With Predictions. Technical Report NASA Technical Note TN D-4578, Research Engineering, NASA Dryden Flight Research Center.

Smith, Ronald H. and Bellman, Donald R. and Hughes, Donald L. (1968) Preliminary Flight Investigation of Dynamic Phenomena Within Air Breathing Propulsion Systems of Supersonic Aircraft. Conference Paper AIAA-1968-593, Research Engineering, NASA Flight Research Center.

Lasagna, Paul L. and McLeod, Norman J. (1968) Preliminary Measured and Predicted XB-70 Engine Noise. Technical Report NASA TM X-1565, 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.

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.

Wilson, Ronald J. and Larson, Richard R. (1967) Statistical Analysis of Landing-Contact Conditions for the XB-70 Airplane. Technical Report NASA Technical Note TN D-4007, Research Engineering, NASA Dryden Flight Research Center.

Powers, Bruce G. (1972) Statistical Survey of XB-70 Airplane Responses and Control Usage With an Illustration of the Application to Handling Qualities Criteria. Technical Report NASA Technical Note TN D-6872, Research Engineering, NASA Dryden Flight Research Center.

Andrews, William H. (1966) Summary of Preliminary Data Derived from the XB-70 Airplanes. Technical Report NASA TM X-1240, Research Engineering, NASA Dryden Flight Research Center.

Wolowicz, Chester H. and Yancey, Roxanah B. (1973) Summary of Stability and Control Characteristics of the XB-70 Airplane. Technical Report NASA TM X-2933, 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.

Arnaiz, Henry H. (1975) Techniques for Determining Propulsion System Forces for Accurate High Speed Vehicle Drag Measurements in Flight. Conference Paper AIAA-1975-964, Research Engineering, NASA Dryden Flight Research Center.

Szalai, Kenneth J. (1971) Validation of a General Purpose Airborne Simulator For Simulation of Large Transport Aircraft Handling Qualities. Technical Report NASA Technical Note TN D-6431, Research Engineering, NASA Dryden Flight Research Center.

Larson, Terry J. and Schweikhard, William G. (1971) Verification of Takeoff Performance Predictions for the XB-70 Airplane. Technical Report NASA TM X-2215, 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.

Putnam, Terrill W. and Smith, Ronald H. (1970) XB-70 Compressor-Noise Reduction and Propulsion-System Performance For Choked Inlet Flow. Technical Report NASA Technical Note TN D-5692, Research Engineering, NASA Dryden Flight Research Center.

This list was generated on Mon Oct 13 18:17:30 PDT 2008.

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