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Computational methods for inlet airframe integrationFundamental equations encountered in computational fluid dynamics (CFD), and analyses used for internal flow are introduced. Irrotational flow; Euler equations; boundary layers; parabolized Navier-Stokes equations; and time averaged Navier-Stokes equations are treated. Assumptions made and solution methods are outlined, with examples. The overall status of CFD in propulsion is indicated.
Document ID
19890007381
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Towne, Charles E.
(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
89N16752
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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