Procedure based upon J.WEISSINGER method presented so that basic span loading, angle of zero lift, and pitching moment due to twist can be readily predicted for wide range of plan forms.
Theoretical basic span loading characteristics of wings with arbitrary sweep, aspect ratio, and taper ratio
Nat Advisory Committee Aeronautics -- Tech Note
1948
33 pages
Illus, Charts, Tables
Report
Englisch
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NTRS | 1988
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