Year: 1950

Number of records: 14.

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 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.

Thompson, Jim Rogers and Roden, William S. and Eggelston, John M. (1950) Flight Investigation of the Aileron Characteristics of the Douglas D-558-I Airplane (BuAero No. 37972) at Mach Numbers Between 0.6 and 0.89. Technical Report NACA RM L50D20, 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.

Wilmerding, J. V. and Stillwell, W. H. and Sjoberg, S. A. (1950) Flight Measurements with the Douglas D-558-II (BuAero No. 37974) Research Airplane Lateral Control Characteristics as Measured in Abrupt Aileron Rolls at Mach Numbers up to 0.86. Technical Report NACA RM L50E17, Research Engineering, NASA Dryden Flight Research Center.

Stillwell, W. H. and Wilmerding, J. V. and Champine, R. A. (1950) Flight Measurements with the Douglas D-558-II (BuAero No. 37974) Research Airplane Low-Speed Stalling and Lift Characteristics. Technical Report NACA RM L50G10, Research Engineering, NASA Dryden Flight Research Center.

Sjoberg, S. A. (1950) Flight Measurements with the Douglas D-558-II (BuAero No. 37974) Research Airplane Static Lateral and Directional Stability Characteristics as Measured in Sideslips at Mach Numbers up to 0.87. Technical Report NACA RM L50C14, Research Engineering, NASA Dryden Flight Research Center.

Sadoff, Melvin and Sisk, Thomas R. (1950) Longitudinal-Stability Characteristics of the Northrop X-4 Airplane (USAF No. 46-677). Technical Report NACA RM A50D27, Research Engineering, NASA Dryden Flight Research Center.

Matthews Jr., James T. (1950) Results Obtained During Flights 1 to 6 of the Northrop X-4 Airplane (A.F. No. 46-677). Technical Report NACA RM L9K22, Research Engineering, NASA Dryden Flight Research Center.

Sadoff, Melvin and Sisk, Thomas R. (1950) Stall Characteristics Obtained from Flight 10 of Northrop X-4 No. 2 Airplane (USAF No. 46-677). Technical Report NACA RM A50A04, Research Engineering, NASA Dryden Flight Research Center.

Sadoff, Melvin and Sisk, Thomas R. (1950) Summary Report of Results Obtained During Demonstration Tests of the Northrop X-4 Airplanes. Technical Report NACA RM A50I01, Research Engineering, NASA Dryden Flight Research Center.

Keener, Earl R. and Pierce, Mary (1950) Tabulated Pressure Coefficients and Aerodynamic Characteristics Measured in Flight on the Wing of the Douglas D-558-I Airplane for a 1g Stall, a Speed Run to a Mach Number of 0.90, and a Wind-Up Turn at a Mach Number of 0.86. Technical Report NACA RM L50J10, 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.

This list was generated on Mon Nov 23 18:17:47 PST 2009.