Aerodynamic study of a wing-fuselage combination employing a wing swept back 63 degrees : effect of sideslip on aerodynamic characteristics at a Mach number of 1.4 with the wing twisted and cambered

Henry C. Lessing
naca-rm-a50f09
Sep 1950


The longitudinal and lateral characteristics of a wing-fuselage combination employing a wing with the leading edge swept back 63 degrees and cambered and twisted for a uniform load at a lift coefficient of 0.25 and at a Mach number of 1.5 are presented. The investigation was carried out through a range of sideslip angles from -5 to 5 degrees at a Mach number of 1.4 at Reynolds numbers of 1.5, 2.7, and 3.7 million.

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