One of most recent and promising solutions of premature stall is use of platform changes involving inverse wing taper, i.e., planform in which tip chord is larger than root chord; reasons for improvement in stall characteristics attending this method; new configuration may be answer to poor stability of swept wing jet fighters and bombers at low speeds.
Theory of inversely tapered wing
Aviation Week
Aviation Week ; 50 , n 12
1949
4 pages
Aufsatz (Zeitschrift)
Englisch
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