Two procedures for calculating lift distribution along span given, in which better account is taken of distribution of circulation over area than in Prandtl lifting line theory. English translation from ZWB Forschungsbericht n 1533 Feb 27 1942.
Lift distribution of swept-back wings
Nat Advisory Committee Aeronautics -- Tech Memo
1947
38 pages
10 Supp plates
Report
Englisch
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Theoretical lift of flat swept-back wings at supersonic speeds
Engineering Index Backfile | 1948
|On chordwise lift distribution at centre of swept wings
Engineering Index Backfile | 1950
|Pressure-distribution measurements on unyawed swept-back wings
Engineering Index Backfile | 1947
|Methods of reducing transonic drag of swept-back wings at zero lift
Engineering Index Backfile | 1957
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