A semi-empirical formula for the prediction of the broadband shock associated noise from rectangular supersonic jets in the fly-over plane has been developed. The predicted noise spectra compared very favorable with the measurement of Ponton, Manning and Seiner. Extension to side-line directions will be carried out.
Climb to Cruise Noise Test Results
01.09.1999
Aufsatz (Konferenz)
Keine Angabe
Englisch
NTRS | 1991