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High-resolution shock-capturing schemes for inviscid and viscous hypersonic flows

Author
Montagne, J.-L.
Published
Apr 1, 1988.
Physical Description
1 electronic document
Additional Creators
Klopfer, G. H. and Yee, H. C.
Online Version

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Unclassified, Unlimited, Publicly available.
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Summary
A class of implicit Total Variation Diminishing (TVD) type algorithms suitable for transonic and supersonic multidimensional Euler and Navier-Stokes equations was extended to hypersonic computations. The improved conservative shock-capturing schemes are spatially second- and third-order, and are fully implicit. They can be first- or second-order accurate in time and are suitable for either steady or unsteady calculations. Enhancement of stability and convergence rate for hypersonic flows is discussed. With the proper choice of the temporal discretization and suitable implicit linearization, these schemes are fairly efficient and accurate for very complex two-dimensional hypersonic inviscid and viscous shock interactions. This study is complimented by a variety of steady and unsteady viscous and inviscid hypersonic blunt-body flow computations. Due to the inherent stiffness of viscous flow problems, numerical experiments indicated that the convergence rate is in general slower for viscous flows than for inviscid steady flows.
Other Subject(s)
Collection
NASA Technical Reports Server (NTRS) Collection.
Note
Document ID: 19880013267.
Accession ID: 88N22651.
A-88148.
NAS 1.15:100097.
NASA-TM-100097.
Terms of Use and Reproduction
No Copyright.
View MARC record | catkey: 15694915