Subject: D-558-II
Number of records: 14.
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.
Fischel, Jack and Reisert, Donald (1956) Effect of Several Wing Modifications on the Subsonic and Transonic Longitudinal Handling Qualities of the Douglas D-558-II Research Airplane. Technical Report NACA RM H56C30, Research Engineering, NASA Dryden Flight Research Center.
Mayer, John P. and Valentine, George M. (1951) Flight Measurements with the Douglas D-558-II (BuAero No. 37974) Research Airplane – Measurements of the Distribution of the Aerodynamic Load Among the Wing, Fuselage, and Horizontal Tail at Mach Numbers up to 0.87. Technical Report NACA RM L50J13, 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.
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.
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.
McLeod, Norman J. and Jordan, Gareth H. (1958) Preliminary Flight Survey of Fuselage and Boundary-Layer Sound-Pressure Levels. Technical Report NACA RM H58B11, Research Engineering, NASA Dryden Flight Research Center.
Sjoberg, Sigurd A. (1949) Preliminary Measurements of the Dynamic Lateral Stability Characteristics of the Douglas D-558-II (BuAero No. 37974) Airplane. Technical Report NACA RM L9G18, 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 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.
(1999) Toward Mach 2: The Douglas D-558 Program, Hunley, J.D., Eds. . National Aeronautics and Space Administration.
This list was generated on Wed Aug 27 18:16:14 PDT 2008.
