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High Resolution Euler Solvers Based on the Space-Time Conservation Element and Solution Element MethodThe I-D, quasi I-D and 2-D Euler solvers based on the method of space-time conservation element and solution element are used to simulate various flow phenomena including shock waves, Mach stem, contact surface, expansion waves, and their intersections and reflections. Seven test problems are solved to demonstrate the capability of this method for handling unsteady compressible flows in various configurations. Numerical results so obtained are compared with exact solutions and/or numerical solutions obtained by schemes based on other established computational techniques. Comparisons show that the present Euler solvers can generate highly accurate numerical solutions to complex flow problems in a straightforward manner without using any ad hoc techniques in the scheme.
Document ID
19980018847
Acquisition Source
Legacy CDMS
Document Type
Contractor Report (CR)
Authors
Wang, Xiao-Yen
(Colorado Univ. Boulder, CO United States)
Chow, Chuen-Yen
(Colorado Univ. Boulder, CO United States)
Chang, Sin-Chung
(NASA Lewis Research Center Cleveland, OH United States)
Date Acquired
September 6, 2013
Publication Date
January 1, 1996
Publication Information
Publisher: American Inst. of Aeronautics and Astronautics
Subject Category
Numerical Analysis
Report/Patent Number
NAS 1.26:207329
AIAA Paper-96-0764
NASA/CR-96-207329
Report Number: NAS 1.26:207329
Report Number: AIAA Paper-96-0764
Report Number: NASA/CR-96-207329
Meeting Information
Meeting: Aerospace Sciences
Location: Reno, NV
Country: United States
Start Date: January 15, 1996
End Date: January 18, 1996
Funding Number(s)
CONTRACT_GRANT: NAG3-1566
Distribution Limits
Public
Copyright
Public Use Permitted.
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