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Cascade with subsonic leading-edge locusThe paper investigates a two-dimensional oscillating cascade with a subsonic leading edge locus in a supersonic flow. The blades are assumed to be of small thickness and camber, and are undergoing small amplitude-harmonic oscillations. The problem is reduced to the solution of a functional integral equation, and an expression is given for the kernel function.
Document ID
19760031026
Acquisition Source
Legacy CDMS
Document Type
Reprint (Version printed in journal)
Authors
Goldstein, M. E.
(NASA Lewis Research Center Cleveland, Ohio, United States)
Date Acquired
August 8, 2013
Publication Date
August 1, 1975
Publication Information
Publication: AIAA Journal
Volume: 13
Subject Category
Aerodynamics
Accession Number
76A13992
Distribution Limits
Public
Copyright
Other

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