It is concluded that delta wing, contrary to widely publicized opinion that it is destined to be wing planform for all future supersonic aircraft, actually offers only limited range of Mach number usefulness, that between 1.0 and 1.4, but this is next important speed regime into which aircraft design is now moving; beyond this speed, however, straight wing is certain to be the answer.
Delta wing
Aero Digest
Aero Digest ; 61 , n 6
1950
12 pages
Bibliography
Aufsatz (Zeitschrift)
Englisch
© Metadata Copyright Elsevier B. V. All rights reserved.
NTIS | 1988
|Engineering Index Backfile | 1951
Tema Archiv | 1985
|Engineering Index Backfile | 1953
|AIAA | 1985
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