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Breakdown of the conservative potential equationThe conservative full-potential equation is used to study transonic flow over five airfoil sections. The results of the study indicate that once shock are present in the flow, the qualitative approximation is different from that observed with the Euler equations. The difference in behavior of the potential eventually leads to multiple solutions.
Document ID
19860010881
Acquisition Source
Legacy CDMS
Document Type
Technical Publication (TP)
Authors
Salas, M. D. (NASA Langley Research Center Hampton, VA, United States)
Gumbert, C. R. (NASA Langley Research Center Hampton, VA, United States)
Date Acquired
September 5, 2013
Publication Date
February 1, 1986
Subject Category
Aerodynamics
Report/Patent Number
L-15769
NASA-TP-2539
NAS 1.60:2539
Report Number: L-15769
Report Number: NASA-TP-2539
Report Number: NAS 1.60:2539
Accession Number
86N20352
Funding Number(s)
PROJECT: RTOP 505-60-01-01
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.

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