Analytical expressions derived for downwash throughout entire induced flow field of lifting triangles of infinite chord with leading edges either in front of or behind Mach cone.
Charts for conical part of downwash field of swept wings at supersonic speeds
Nat Advisory Committee Aeronautics -- Tech Note
1948
32 pages
Report
Englisch
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Charts for estimating downwash behind rectangular, trapezoidal, and triangular wings at supersonic
Engineering Index Backfile | 1950
|Calculation of downwash behind wings of arbitrary plan form at supersonic speeds
Engineering Index Backfile | 1950
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