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Effects of Symmetric and Asymmetric Thrust Reversal on the Aerodynamic Characteristics of a Model of a Twin-engine Airplane (1953)

NASA Technical Reports Server (NTRS) · leaf 57

An illustration from Effects of Symmetric and Asymmetric Thrust Reversal on the Aerodynamic Characteristics of a Model of a Twin-engine Airplane, 1953, leaf 57 — MCA TN 2979 56 I < Pitching-moment coefficient, C, V Angie of attack, a, deg (a) Concluded. Figure 26.- Continued

NASA Technical Reports Server (NTRS)

Internet Archive · NASA Technical Reports · Public domain (US government work). Free to use for anything.

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