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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 52
% i $ Ja Asymmetric,TCr= 0.167 [□ Asymmetric, TCr =0063 … (b) Effect of asymmetric thrust coefficient on aerodynamic characteristics. Figure 23.- Concluded. VJINASA Technical Reports Server (NTRS)
Internet Archive · NASA Technical Reports · Public domain (US government work). Free to use for anything.
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