Transonic flight test to compare the zero-lift drag of underslung and symmetrical nacelles varied chordwise at 40 percent semispan of a 45 degree sweptback, tapered wing

Pepper, William B , Jr Hoffman, Sherwood
naca-rm-l50g17a
October 25, 1950


No Abstract Available

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http://naca.central.cranfield.ac.uk/reports/1950/naca-rm-l50g17a.pdf