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CFD application to subsonic inlet airframe integrationThe fluid dynamics of curved diffuser duct flows of military aircraft is discussed. Three-dimensional parabolized Navier-Stokes analysis, and experiment techniques are reviewed. Flow measurements and pressure distributions are shown. Velocity vectors, and the effects of vortex generators are considered.
Document ID
19890007382
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Anderson, Bernhard H. (NASA Lewis Research Center Cleveland, OH, United States)
Date Acquired
September 5, 2013
Publication Date
January 1, 1988
Publication Information
Publication: VKI, Intake Aerodynamics, Volume 2
Subject Category
Aerodynamics
Accession Number
89N16753
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.

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