Subject: XF-92

• Subject Areas (1620)
  • Aircraft/Project (1292)
    • XF-92 (9)

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Number of records: 9.

Holleman, Euclid C. (1955) Flight Measurements of the Lateral Response Characteristics of the Convair XF-92A Delta-Wing Airplane. Technical Report NACA RM H55E26, 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.

Sisk, Thomas R. and Muhleman, Duane O. (1955) Lateral Stability and Control Characteristics of the Convair XF-92A Delta-Wing Airplane as Measured in Flight. Technical Report NACA RM H55A17, Research Engineering, NASA Dryden Flight Research Center.

Brunn, Cyril D. and Stillwell, Wendell H. (1956) Mach Number Measurements and Calibrations During Flight at High Speeds and at High Altitudes Including Data for the D-558-II Research Airplane. Technical Report NACA RM H55J18, 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.

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.

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.

This list was generated on Mon Nov 23 18:17:32 PST 2009.