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Analytical study of twin-jet shieldingProgress in the refinement and evaluation of an analytical jet shielding model are summarized. The model consists of a point noise source impinging on a cylinder of heated flow in which the temperature and velocity are uniform across the cross section of the jet. The shielding jet is infinite in extent along the jet axis and the radius of the jet is constant. The analytical model was compared to experimental data for a point noise source impinging on an ambient temperature, subsonic jet and on a subsonic simulated hot jet using helium as the flow medium. Results of these comparisons are discussed.
Document ID
19820008927
Acquisition Source
Legacy CDMS
Document Type
Contractor Report (CR)
Authors
Gerhold, C. H.
(Texas A&M Univ. College Station, TX, United States)
Date Acquired
September 4, 2013
Publication Date
January 1, 1982
Subject Category
Acoustics
Report/Patent Number
NASA-CR-165102
APR-2
Report Number: NASA-CR-165102
Report Number: APR-2
Accession Number
82N16801
Funding Number(s)
CONTRACT_GRANT: NAG1-11
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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