Pressure distributions at Mach numbers of 1.6 and 1.9 of a conically cambered wing of triangular plan form with and without pylon-mounted engine nacelles

Phelps, E. Ray.
naca-rm-a56b03
1956


Results are presented of an experimental investigation of the pressure-distribution characteristics of a conically cambered wing of triangular plan form with and without four pylon-mounted engine nacelles. The experimental investigation was conducted at Mach numbers of 1.6 and 1.9 for Reynolds numbers of 2.9 and 2.6 million, respectively.

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