Experimental Study of the Supersonic Flow Around V-Shaped Wings

Unedited machine trans. of Trudy Nauchnoy Mekhanicheskiy Institut Universiteta Moskva (USSR) n1 p58-70 1970.

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Bibliographic Details
Main Authors: Gonor,A L, Kazakov,M N, Shvets,A I
Format: Report
Language:English
Subjects:
AERODYNAMIC CONFIGURATIONS
Aircraft
CROSS SECTIONS
Fluid Mechanics
LIFT TO DRAG RATIO
SUPERSONIC FLOW
TRANSLATIONS
USSR
V wings
WINGS
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Summary:Unedited machine trans. of Trudy Nauchnoy Mekhanicheskiy Institut Universiteta Moskva (USSR) n1 p58-70 1970.