Mathematical investigation of factors controlling stability in nose-steered or tail-first airplane by means of simplified formulas for moment coefficient of wing; slope of moment line of wing; moment coefficient of horizontal empennage; including area, chord and angle of attack of wing. From Zeit. fuer Flugtechnik und Motorluftschiffahrt, Dec. 15, 1930, indexed in Engineering Index 1930, p. 67.
Static longitudinal stability of "Ente" airplanes
Nat. Advisory Committee Aeronautics -- Tech. Memorandum
1930
27 pages
21 Figs.
Report
English
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Static longitudinal stability of "Ente" airplanes
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