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Shock structure in transonic compressor rotorsThe inadequacy of axisymmetric theory in modeling the structure of the shock system in a transonic compressor rotor is shown with a simple model. A more accurate model for the flow near the sonic radius is proposed, which is supported by some flow visualization data and three-dimensional computations.
Document ID
19790046589
Acquisition Source
Legacy CDMS
Document Type
Reprint (Version printed in journal)
Authors
Epstein, A. H. (Massachusetts Inst. of Tech. Cambridge, MA, United States)
Kerrebrock, J. L. (Massachusetts Inst. of Tech. Cambridge, MA, United States)
Thompkins, W. T., Jr. (MIT Cambridge, Mass., United States)
Date Acquired
August 9, 2013
Publication Date
April 1, 1979
Publication Information
Publication: AIAA Journal
Volume: 17
Subject Category
Aerodynamics
Accession Number
79A30602
Funding Number(s)
CONTRACT_GRANT: NGL-22-009-383
Distribution Limits
Public
Copyright
Other

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