Year: 1955

Number of records: 21.

Dryden, Hugh L. and Duberg, Dr. John E. (1955) Aeroelastic Effects of Aerodynamic Heating. Technical Paper AGARD GA5/8, Research Engineering, NASA Dryden Flight Research Center.

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.

Fischel, Jack and Reisert, Donald (1955) Effect of Several Wing Modifications on the Low-Speed Stalling Characteristics of the Douglas D-558-II Research Airplane. Technical Report NACA RM H55E31a, Research Engineering, NASA Dryden Flight Research Center.

Thompson, Jim Rogers and Bray, Richard S. and Cooper, George E. (1955) Flight Calibration of Four Airspeed Systems on a Swept-Wing Airplane at Mach Numbers up to 1.04 by the NACA Radar-Phototheodolite Method. Technical Report NACA TN 3526, Research Engineering, NASA Dryden Flight Research Center.

Finch, Thomas W. (1955) Flight Determination of the Longitudinal Stability and Control Characteristics of the Bell X-5 Research Airplane at 58.7 Degrees Sweepback. Technical Report NACA RM H55C07, Research Engineering, NASA Dryden Flight Research Center.

Weil, Joseph and Gates Jr., Ordway B. and Banner, Richard D. and Kuhl, Albert E. (1955) Flight Experience of Inertia Coupling in Rolling Maneuvers. Technical Report NACA RM H55E17b, Research Engineering, NASA Dryden Flight Research Center.

Sisk, Thomas R. and Andrews, William H. (1955) Flight Experience with a Delta-Wing Airplane Having Violent Lateral-Longitudinal Coupling in Aileron Rolls. Technical Report NACA RM H55H03, Research Engineering, NASA Dryden Flight Research Center.

Staff, NACA (1955) Flight Experience with Two High-Speed Airplanes Having Violent Lateral-Longitudinal Coupling in Aileron Rolls. Technical Report NACA RM H55A13, Research Engineering, NASA Dryden Flight Research Center.

Drake, Hubert M. and Finch, Thomas W. and Peele, James R. (1955) Flight Measurements of Directional Stability to a Mach Number of 1.48 for an Airplane Tested with Three Different Vertical Tail Configurations. Technical Report NACA RM H55G26, Research Engineering, NASA Dryden Flight Research Center.

Reed, Robert D. (1955) Flight Measurements of Horizontal-Tail Loads on the Bell X-5 Research Airplane at a Sweep Angle of 58.7 Degrees. Technical Report NACA RM H55E20a, Research Engineering, NASA Dryden Flight Research Center.

Videan, Edward N. (1955) Flight Measurements of the Dynamic Lateral and Longitudinal Stability of the Bell X-5 Research Airplane at 58.7 Degrees Sweepback. Technical Report NACA RM H55H10, Research Engineering, NASA Dryden Flight Research Center.

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.

Jordan, Gareth H. and Keener, Earl R. (1955) Flight-Determined Pressure Distributions Over a Section of the 35 Degree Swept Wing of the Douglas D-558-II Research Airplane at Mach Numbers up to 2.0. Technical Report NACA RM H55A03, 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.

Jordan, Gareth H. and Hutchins Jr., C. Kenneth (1955) Preliminary Flight-Determined Pressure Distributions Over the Wing of the Douglas X-3 Research Airplane at Subsonic and Transonic Mach Numbers. Technical Report NACA RM H55A10, 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.

Day, Richard E. and Fischel, Jack (1955) Stability and Control Characteristics Obtained During Demonstration of the Douglas X-3 Research Airplane. Technical Report NACA RM H55E16, Research 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.

Banner, Richard D. and Reed, Robert D. and Marcy, William L. (1955) Wing-Load Measurements of the Bell X-5 Research Airplane at a Sweep Angle of 58.7 Degrees. Technical Report NACA RM H55A11, Research Engineering, NASA Dryden Flight Research Center.

This list was generated on Wed Aug 27 18:17:48 PDT 2008.