Supersonic Jet Noise: Its Generation, Prediction and Effects on People and Structures 901927
This paper presents the results of a study aimed at quantifying the effects of jet source noise reduction, increases in aircraft lift, and reduced aircraft thrust on the take-off noise associated with supersonic civil transports. Supersonic jet noise sources are first described, and their frequency and directivity dependence are defined. The study utilizes NASA's Aircraft Noise Prediction Program (ANOPP) in a parametric study to weigh the relative benefits of several approaches to low noise. The baseline aircraft concept used in these predictions is the AST-205-1 powered by GE21/J11-B14A scaled engines. Noise assessment is presented in terms of effective perceived noise levels (EPNL) at the FAA's centerline and sideline measuring locations for current subsonic aircraft, and in terms of audiologically perceived sound of people and other indirect effects. The results show that significant noise benefit can be achieved through proper understanding and utilization of all available approaches.
Citation: Preisser, J., Golub, R., Seiner, J., and Powell, C., "Supersonic Jet Noise: Its Generation, Prediction and Effects on People and Structures," SAE Technical Paper 901927, 1990, https://doi.org/10.4271/901927. Download Citation
J. S. Preisser, R. A. Golub, J. M. Seiner, C. A. Powell
NASA Langley Research Center Hampton, Virginia
Aerospace Technology Conference and Exposition
SAE Transactions - Journal of Aerospace-V99-1