A study of factors affecting the steady spin of an airplane (1933)
NASA Technical Reports Server (NTRS) · leaf 23
Figs N.A.C.A. Technical Note No.468 .12 - i i—i 1 > 1—i—i [— V= - 85" Aerodynamic moment 20 30 40 SO 60 Angle of attack, degrees Figure 3.-Computed aerodynamic and gyroscopic roll- ing moment coefficients, elevator up 33° . … Angle of attack, degrees Figure 4.-Computed aerodynamic and gyroscopic pitching- moment coefficients,elevator up 33° .
NASA Technical Reports Server (NTRS)
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