Static pressure coefficient distributions on the forebody, afterbody, and nozzles of a 1/12 scale F-15 propulsion model were determined. The effects of nozzle power setting and horizontal tail deflection angle on the pressure coefficient distributions were investigated.
Fuselage and nozzle pressure distributions on a 1/12-scale F-15 propulsion model at transonic speeds
1979-11-01
Report
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English