Research Catalog

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

Title
Noise computation of a shock-containing supersonic axisymmetric jet by the CE/SE method [microform] / Ching Y. Loh ... [et al.].
Publication
[Cleveland, Ohio] : National Aeronautics and Space Administration, Glenn Research Center ; [Springfield, Va. : National Technical Information Service, distributor, 1999]

Details

Additional Authors
  • Loh, Ching Y.
  • NASA Glenn Research Center.
Description
1 v.
Series Statement
[NASA technical memorandum] ; NASA/TM-1999-209658
Uniform Title
NASA technical memorandum ; 209658.
Alternative Title
Noise computation of a shock containing supersonic axisymmetric jet by the CE/SE method
Subject
  • Supersonic jet flow
  • Aeroacoustics
  • Jet aircraft noise
  • Mechanical shock
  • Noise measurement
Note
  • Shipping list no.: 2000-0603-M.
Reproduction (note)
  • Microfiche.
Call Number
READEX Microfiche NAS 1.15:209658
OCLC
marcive44558579
Title
Noise computation of a shock-containing supersonic axisymmetric jet by the CE/SE method [microform] / Ching Y. Loh ... [et al.].
Imprint
[Cleveland, Ohio] : National Aeronautics and Space Administration, Glenn Research Center ; [Springfield, Va. : National Technical Information Service, distributor, 1999]
Series
[NASA technical memorandum] ; NASA/TM-1999-209658
NASA technical memorandum ; 209658.
Reproduction
Microfiche. [Washington, D.C. : National Aeronautics and Space Administration, 2000] 1 microfiche.
Added Author
Loh, Ching Y.
NASA Glenn Research Center.
Gpo Item No.
0830-D (MF)
Sudoc No.
NAS 1.15:209658
Research Call Number
READEX Microfiche NAS 1.15:209658
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