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Report (1915)

United States. National Advisory Committee for Aeronautics, United States. National Aeronautics and Space Administration · Washington : G.P.O. · leaf 670

An illustration from Report, 1915, leaf 670
1.25, which is somewhnl. simdier (.hiiu 1 he load factor found wilhan acc(>ler()met(>r in similar spins. Il is pi-ohahle Ihal. (he principal cause of the discrepancir-Hlies in i,\\c fact thai. Mie ailerons are nol. centered, and that the actual coedicient of normalforco on the outer [)ortion… … 100 7 .6 90 .4 o o GO \ V .2 70 -32 -20 -/2 -8-4 O -^4 *8 */2 Oisfonce from F/ane of Symmetry /h Feet. FiR. 7. *20 *22 :^.0 60 It will be noted in figure 7 that the resultant speed does not by any means vary uniformlyalong the wing, })ut falls off to a minimum just beyond the inner strut on the…

Aeronautics

Internet Archive · Gerstein Library, University of Toronto · Public Domain Mark 1.0. Free to use for anything.

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