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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 waves 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
19850037549
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Salas, M. D.
(NASA Langley Research Center Hampton, VA, United States)
Gumbert, C. R.
(NASA Langley Research Center Transonic Aerodynamics Div., Hampton, VA, United States)
Date Acquired
August 12, 2013
Publication Date
January 1, 1985
Subject Category
Aerodynamics
Report/Patent Number
AIAA PAPER 85-0367
Report Number: AIAA PAPER 85-0367
Accession Number
85A19700
Distribution Limits
Public
Copyright
Other

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