Theoretical study of aerodynamic characteristics at zero angle of attack of thin, doubly symmetrical double wedge profile in range of supersonic flight speed in which bow wave is detached. Supersedes NAC A -- Tech Notes 2339 and 2588.
Transonic flow past wedge profile with detached bow wave
NACA -- Report
1952
30 pages
Report
English
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Transonic flow past a wedge profile with detached bow wave
TIBKAT | 1952
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Engineering Index Backfile | 1951
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