Data presentation of force characteristics of several engine-strut-body configurations at Mach numbers of 1.8 and 2.0

Robert T. Madden, Emil J. Kremzier
naca-rm-e51e29
Aug 1951


Lift, drag, and pitching-moment characteristics obtained from an investigation of several engine-strut-body combinations in the NACA Lewis 8- by 6-foot supersonic wind tunnel are presented for Mach numbers of 1.8 and 2.0 and a range of angle of attack from 0 to 10 degrees.

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