Noise computation of a shock-containing supersonic axisymmetric jet by the CE/SE method /

Bibliographic Details

Main Author:	Loh, Ching Y. (Ching Yuen), 1944- (Author)
Format:	Government Document eBook
Language:	English
Published:	Cleveland, Ohio : National Aeronautics and Space Administration, Glenn Research Center, December 1999.
Series:	NASA technical memorandum ; 1999-209658.
Subjects:	Supersonic jet flow. Aeroacoustics. Jet aircraft noise. Mechanical shock. Noise measurement.
Online Access:	https://purl.fdlp.gov/GPO/gpo84793