Noise computation of a shock-containing supersonic axisymmetric jet by the CE/SE method
By: Ching Y. Loh ... [et al.].
Contributors: Loh, Ching Y.; NASA Glenn Research Center.
Series: [NASA technical memorandum] -- NASA/TM-1999-209658.; NASA technical memorandum -- 209658.
Publisher: National Aeronautics and Space Administration, Glenn Research Center; National Technical Information Service, distributor
Published: 1999
Place of publication: [Cleveland, Ohio]; [Springfield, Va
Language: eng
Format: Microform
Subjects: Supersonic jet flow.; Aeroacoustics.; Jet aircraft noise.; Mechanical shock.; Noise measurement.
Other titles: Noise computation of a shock containing supersonic axisymmetric jet by the CE/SE method.
Notes: Shipping list no.: 2000-0603-M.

Microfiche. [Washington, D.C. : National Aeronautics and Space Administration, 2000] 1 microfiche.