Forward flight effects on broadband shock associated noise of supersonic jetsThe stochastic model theory of TAM (1987, 1989) for broadband shock associated noise was extended to include the effects of forward flight. The theory was applied to the forward flight simulation experiments of Norum and Shearin (1984, 1986, and 1988). Good agreement is found between calculated and measured far-field noise spectra over the flight Mach number range of 0.0 to 0.4.
Document ID
19890046358
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Tam, Christopher K. W. (Florida State University Tallahassee, United States)