Similarity laws governing relationship between relative profile thickness and free stream Mach number for similar pressure distributions have long been known for plane transonic flow around thin airfoils; these similarity laws are now generalized to be valid for wings of finite aspect ratio.
Similarity laws for transonic flow around wings of finite aspect ratio
Stockholm, Kungl. Tekniska Hogskolan -- Inst Flygteknik (Roy Inst Technology -- Div Aeronautics) TN
1950
8 pages
Aufsatz (Zeitschrift)
Englisch
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Similarity laws for transonic flow about wings of finite span
TIBKAT | 1951
|Similarity laws for transonic flow about wings of finite span
Engineering Index Backfile | 1951
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