Method is developed for calculating spanwise lift distribution and other aerodynamic characteristics of simple wing; effects of landing flap displacement and aileron displacement considered; worked numerical examples are given in order to explain application as well as to check accuracy of method.
Simple method of calculating aerodynamic characteristics of monoplane wing
Tokyo Imperial Univ -- Aeronautical Research Inst -- Report
1940
87 pages
Bibliography
Aufsatz (Zeitschrift)
Englisch
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