Stability in aviation : an introduction to dynamical stability as applied to the motions of aeroplanes (1911)
Bryan, George Hartley, 1864-1928 · London : Macmillan · leaf 175
LATERAL STABILITY 159 VIII Taking Fig. .37 as representing the seetion uf the wings in the plane of {y, z), R any point on the wing on the positive side of the plane of {x, y), GQ a perpendicular on the wing AP produced, let RP = p, PQ = e, so that RQ = z cos fi - ;/ sin i3 - p + e, RP = :. sec /3… … With this notation the determinantal equation becomes _ W _W sin 6 fKUy\ W cos d/KU<j\ /"sin^ ^(/,S" + T, + 'Kg KW^g\ X KUg + 2 ffjip sin (i cos ^dS' - xT, - Up + e) sin ^dS\ FX^ - |(p + e) sin ^dS', KUg KUg -2 I ppip + e) COS ^dS', BX Up sin IS cos ^dS' - xT, + x'-T KUg KUg jfipip + e) cos fidS',…
Stability of aeroplanes
Internet Archive · Gerstein - University of Toronto · Public domain (published before 1931). Free to use for anything.
