Pressure and Temperature for B-1B Transparency Test
Technical memo. Feb 1990-Apr 1991
WRIGHT LAB WRIGHT-PATTERSON AFB OH
Pagination or Media Count:
Pressure and temperature data are presented for life cycle testing of the B-lB transparency. For each of three mission types, contour plots of pressure and temperature are presented for each mission segment. Potential flow theory was used to calculate pressure. Isentropic flow was assumed for calculating temperature.