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On the transfer of energy to an unstable liquid jet in a coflowing compressible airstreamThe transfer of energy from a compressible airstream to a coflowing unstable liquid jet via the pressure perturbation at the interface is studied as the Mach number varies continuously from subsonic to supersonic values. The 'lift' component of the pressure perturbation has been demonstrated to predominate up to slightly supersonic free-stream Mach numbers, after which the 'drag' component predominates.
Document ID
19930055399
Acquisition Source
Legacy CDMS
Document Type
Reprint (Version printed in journal)
External Source(s)
doi:10.1063/1.858615
Authors
Li, Hsi-Shang (NASA Ames Research Center Moffett Field, CA, United States)
Kelly, Robert E. (California Univ. Los Angeles, United States)
Date Acquired
August 16, 2013
Publication Date
May 1, 1993
Publication Information
Publication: Physics of Fluids A
Volume: 5
Issue: 5
ISSN: 0899-8213
Subject Category
Fluid Mechanics And Heat Transfer
Accession Number
93A39396
Funding Number(s)
CONTRACT_GRANT: NCC2-374
Distribution Limits
Public
Copyright
Other

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