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On the Kernel function for the unsteady supersonic cascade with subsonic leading edge locusA function integral equation governing the unsteady motion of a supersonic cascade is derived. Various representations of the Kernel function are derived and discussed.
Document ID
19750009540
Acquisition Source
Legacy CDMS
Document Type
Technical Memorandum (TM)
Authors
Goldstein, M. E. (NASA Lewis Research Center Cleveland, OH, United States)
Date Acquired
September 3, 2013
Publication Date
February 1, 1975
Subject Category
Fluid Mechanics And Heat Transfer
Report/Patent Number
E-8220
NASA-TM-X-71673
Report Number: E-8220
Report Number: NASA-TM-X-71673
Accession Number
75N17612
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.

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