Second-Order Methods in Inviscid Supersonic Theory
Author:
Affiliation:
1. Armaments Division, Sir W. G. Armstrong Whitworth Aircraft, Limited, Baginton, near Coventry, England
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Link
http://arc.aiaa.org/doi/pdf/10.2514/8.3240
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5. THE EFFECT OF HEAT TRANSFER ON THE SEPARATION OF A COMPRESSIBLE LAMINAR BOUNDARY LAYER
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1. A boundary layer theory for the buckling of thin cylindrical shells under external pressure;Applied Mathematics and Mechanics;1988-06
2. An Introduction to Second-Order Wing Theory;Journal of the Aeronautical Sciences;1957-02
3. Visualization of Low-Density Flows by Means of Oxygen Absorption of Ultraviolet Radiation;Journal of the Aeronautical Sciences;1957-02
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