Subject: X-1

• Subject Areas (1489)
  • Aircraft/Project (1219)
    • X-1 (17)

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Number of records: 17.

Drake, Hubert M. and Stillwell, Wendell H. (1955) Behavior of the Bell X-1A Research Airplane During Exploratory Flights at Mach Numbers Near 2.0 and at Extreme Altitudes. Technical Report NACA RM H55G25, Research Engineering, NASA Dryden Flight Research Center.

Angle, Ellwyn E. and Holleman, Euclid C. (1950) Determination of Longitudinal Stability of the Bell X-1 Airplane from Transient Responses at Mach Numbers up to 1.12 at Lift Coefficients of 0.3 and 0.6. Technical Report NACA RM L50I06a, Research Engineering, NASA Dryden Flight Research Center.

Drake, Hubert M. (1950) Effects on the Lateral Oscillation of Fixing the Rudder and Reflexing the Flaps on the Bell X-1 Airplane. Technical Report NACA RM L50I05, 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.

Drake, Hubert M. and Carden, John R. (1950) Elevator-Stabilizer Effectiveness and Trim of the X-1 Airplane to a Mach Number of 1.06. Technical Report NACA RM L50G20, 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.

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.

Drake, Hubert M. (1949) Measurements of Aileron Effectiveness of the Bell X-1 Airplane at Mach Numbers Between 0.9 and 1.06. Technical Report NACA RM L9G19a, 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.

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.

Stillwell, Wendell H. and Drake, Hubert M. (1958) Simulator Studies of Jet Reaction Controls For Use at High Altitude. Technical Report NACA RM H58G18A, 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 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.

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.

Love, James E. and Stillwell, Wendell H. (1959) The Hydrogen-Peroxide Rocket Reaction-Control System for the X-1B Research Airplane. Technical Report NASA Technical Note TN D-185, Research Engineering, NASA Dryden Flight Research Center.

This list was generated on Mon Oct 13 18:17:14 PDT 2008.