Universally applicable, rule-of-thumb law for transonic design established by National Advisory Committee for Aeronautics; rule is based on idea that drag of wing/body combination could be reduced by remolding fuselage to follow local streamlines; rule applies to any form of body designed to pass through transonic regime. (See also Flight v 68 n 2436 Sept 30 1955 p 549-52; Engineering v 180 n 4690 Dec 16 1955 p 812-3)
Area rule
Shell Aviation News
Shell Aviation News ; n 213
1956
3 pages
Aufsatz (Zeitschrift)
Englisch
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Engineering Index Backfile | 1955
Engineering Index Backfile | 1955
NTIS | 1977
|AIAA | 1963
|Engineering Index Backfile | 1958
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