Publication Date:
2019-06-27
Description:
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.
Keywords:
AERODYNAMICS
Type:
NASA-TP-1521
,
L-12948
Format:
application/pdf