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Static longitudinal stability of "Ente" airplanes (1931)
NASA Technical Reports Server (NTRS) · leaf 35
N.A.CAi Technical Memorand\im No.613 Figs.17^18 8;5 -0.1 Fig.17 a j^p^/a Q plotted aga,inst O.G. loca.tion r/t. ^ niFo ^ mHq a- 0 ; Hq -140-12°-100-30 -6^-4° -2° 0° … r/t=,3 Fig.18 Determination of stability characteristics of profile combinations for wing and empennage, ^iFq = f(a o); a = ^^^Hq^)-NASA Technical Reports Server (NTRS)
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