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Recent developments in transonic Euler flow over a circular cylinderNumerical solutions to the Euler equations for transonic flow over a circular cylinder indicate that the inviscid flow separates ahead of the rear stagnation point. This phenomenon and various solutions related to this subject are discussed.
Document ID
19820016982
Acquisition Source
Legacy CDMS
Document Type
Technical Memorandum (TM)
Authors
Salas, M. D. (NASA Langley Research Center Hampton, VA, United States)
Date Acquired
September 4, 2013
Publication Date
April 1, 1982
Subject Category
Numerical Analysis
Report/Patent Number
NASA-TM-83282
NAS 1.15:83282
Report Number: NASA-TM-83282
Report Number: NAS 1.15:83282
Accession Number
82N24858
Funding Number(s)
PROJECT: RTOP 505-31-13-01
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.

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