Proceeding from fundamental problem on mutual relation of wing and free boundaries, distribution of circulation is determined for airfoil spaning open jet of rectangular section at different aspect ratios, and then for open jet of circular section; solution obtained by means of Fourier series; experiments performed for purpose of proving theory.
Airfoil spanning open jet
Nat Advisory Committee Aeronautics -- Tech Memo
1933
22 pages
9 Supp sheets
Report
English
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