Simple method suggested for design of wings whose aerodynamic center is independent of variation of lateral dimensions of wing; method applied to tapered wings, and good agreement found with tests on wings with straight trailing edges, and taper ratio of 0.303.
Note on position of aerodynamic center of pointed wings at subsonic speeds
Stockholm. Kungl. Tekniska Hogskolan -- Inst Flygteknik -- Tech Note
1949
6 pages
Report
Englisch
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