Transonic Flight Tests To Compare The Zero Lift Drag Of Underslung And Symmetrical Nacelles Varied Chordwise At 40 Percent Semispan Of A 45 Degrees Sweptback Tapered Wing

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Longitudinal Stability Characteristics at Transonic Speeds of a Rocket-propelled Model of an Airplane Having a 45 Degree Swept Wing of Aspect Ratio 6.0
Language: en
Pages: 44