Theoretical calculation of pressure distribution, span loading, and rolling moment due to sideslip at supersonic speeds for thin sweptback tapered wings with supersonic trailing edges and wing tips parallel to axis of wing symmetry.
Theoretical calculation of pressure distribution, span loading, and rolling moment due to sideslip at supersonic speeds for thin sweptback tapered wings with supersonic trailing edges and wing tips parallel to axis of wing symmetry
NACA -- Tech Note
1953
70 pages
Report
English
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