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Unsteady Transonic Small Disturbance theory with strong shock wavesTransonic Small Disturbance (TSD) theory is modified to yield steady and unsteady solutions in the case of strong shock waves (where the local Mach number ahead of the shock exceeds 1.3). The modification consists of an additional adjustable nonlinear term which allows the exact Rankine-Hugoniot shock jump relation to be satisfied at all times. The modified TSD theory is applied to steady and unsteady oscillatory transonic flows, and yields results which are in good agreement with solutions of the unsteady Euler equations, and which compare favorably with solutions of the full potential equation when shock waves are weak.
Document ID
19820034277
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Kerlick, G. D.
(Nielsen Engineering and Research, Inc. Mountain View, CA, United States)
Nixon, D.
(Nielsen Engineering and Research, Inc. Mountain View, CA, United States)
Ballhaus, W. F., Jr.
(NASA Ames Research Center Moffett Field, CA, United States)
Date Acquired
August 10, 2013
Publication Date
January 1, 1982
Subject Category
Aerodynamics
Report/Patent Number
AIAA PAPER 82-0159
Meeting Information
Meeting: Aerospace Sciences Meeting
Location: Orlando, FL
Start Date: January 11, 1982
End Date: January 14, 1982
Sponsors: American Institute of Aeronautics and Astronautics
Accession Number
82A17812
Distribution Limits
Public
Copyright
Other

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