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

Noise computation of a shock-containing supersonic axisymmetric jet by the CE/SE method [microform] / Ching Y. Loh [and others]

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Bibliographic Details
Corporate Author: NASA Glenn Research Center
Other Authors: Loh, Ching Y. (Ching Yuen), 1944-
Format: Government Document Microfilm Book
Language:English
Published: [Cleveland, Ohio] : [Springfield, Va.] : National Aeronautics and Space Administration, Glenn Research Center ; [National Technical Information Service, distributor], [1999]
Series:NASA technical memorandum ; 209658.
Subjects:
Supersonic jet flow.
Aeroacoustics.
Jet aircraft noise.
Mechanical shock.
Noise measurement.

Norlin Library - Government Information - Microform

Holdings details from Norlin Library - Government Information - Microform
Call Number: NAS 1.15:209658
NAS 1.15:209658 Restricted Place a Hold

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