NASA Logo

NTRS

NTRS - NASA Technical Reports Server

Press Enter or click the Search button to begin your search.

Back to Results
Application of the space-time conservation element and solution element method to shock-tube problemAn Euler solver based on the method of space-time conservation element and solution element is in this paper to simulate shock-tube flows involving shock waves, contact discontinuities, expansion waves and their intersections. Seven test problems are considered to examine the capability of this method. The numerical results, when compared with exact solutions and/or numerical solutions by other methods, indicate that the present method can accurately resolve strong shock and contact discontinuities without using any ad hoc techniques which are used only at the neighborhood of a discontinuity.
Document ID
19950010488
Acquisition Source
Legacy CDMS
Document Type
Technical Memorandum (TM)
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
December 1, 1994
Subject Category
Fluid Mechanics And Heat Transfer
Report/Patent Number
E-9288
NASA-TM-106806
NAS 1.15:106806
Report Number: E-9288
Report Number: NASA-TM-106806
Report Number: NAS 1.15:106806
Accession Number
95N16903
Funding Number(s)
PROJECT: RTOP 505-62-52
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
No Preview Available