A System for aerodynamic design and analysis of supersonic aircraft
Corporate Authors: | United States National Aeronautics and Space Administration Scientific and Technical Information Branch, United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch, Langley Research Center |
---|---|
Other Authors: | Middleton, W. D., Lundry, J. L., Coleman, R. G. |
Format: | Book |
Language: | English |
Published: |
Test cases Washington, D.C.:
National Aeronautics and Space Administration, Scientific and Technical Information Branch,
1980
|
Series: | NASA contractor report
NASA CR-3351-NASA CR-3354 |
Subjects: |
Similar Items
-
Estimation of wing nonlinear aerodynamic characteristics at supersonic speeds/
by: Carlson, Harry W.
Published: (1980) -
Supersonic aerodynamics of delta wings/
by: Wood, Richard M.
Published: (1988) -
Effect of leading-edge load constraints on the design and performance of supersonic wings/
by: Darden, Christine M.
Published: (1985) -
A wing concept for supersonic maneuvering/
by: Mason, William H. 1947-
Published: (1983) -
Experimental and theoretical supersonic lateral-directional stability characteristics of a simplified wing-body configuration with a series of vertical-tail arrangements/
by: Lamb, Milton
Published: (1981)