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Fully implicit shock trackingA tracking method for solving hyperbolic free boundary problems arising in fluid dynamics is presented. The principal feature of the new approach is that the implicit form is used to simultaneously treat both interior points and boundary conditions. In particular, the location of the free boundary (shock) surface is treated implicitly and coupled with all other unknowns. The method is presented in the context of unsteady one-dimensional flow in a variable area duct with an internal shock wave. The fully implicit method and other strategies for advancing the shock are compared for computing a steady solution via a time asymptotic approach. Issues regarding extension of the method to multiple dimensions are also discussed.
Document ID
19810025321
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Bell, J. B.
(Naval Surface Weapons Center Silver Spring, MD, United States)
Shubin, G. R.
(Naval Surface Weapons Center Silver Spring, MD, United States)
Solomon, J. M.
(Naval Surface Weapons Center Silver Spring, MD, United States)
Date Acquired
August 11, 2013
Publication Date
October 1, 1981
Publication Information
Publication: NASA. Ames Research Center Numerical Boundary Condition Procedures
Subject Category
Numerical Analysis
Accession Number
81N33864
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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