Comparison between experimental pressure distributions on inclined model airship hull and those calculated by nonviscous theory; problem is of more interest at present to missile and supersonic aircraft designers.
Pressure distribution and some effects of viscosity on slender inclined bodies of revolution
Nat Advisory Committee Aeronautics -- Tech Note
1950
19 pages
Diagrs, Charts
Report
Englisch
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Hypersonic minimum-drag slender bodies of revolution
AIAA | 1966
|Hypersonic minimum-drag slender bodies of revolution.
AIAA | 1966
|