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
140 pages
Report
No indication
English