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3 edition of High-resolution shock-capturing schemes for inviscid and viscous hypersonic flows found in the catalog.

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

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

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  • 26 Currently reading

Published by National Aeronautics and Space Administration, Ames Research Center in Moffet Field, Calif .
Written in English

    Subjects:
  • Fluid dynamics.,
  • Aerodynamics, Hypersonic.

  • Edition Notes

    Other titlesHigh resolution shock capturing schemes for inviscid and viscous hypersonic flows
    StatementH.C. Yee, G.H. Klopfer, J.-L. Montagne.
    SeriesNASA technical memorandum -- 100097
    ContributionsKlopfer, Goetz H., Montagne, J.-L., Ames Research Center.
    The Physical Object
    FormatMicroform
    Pagination1 v.
    ID Numbers
    Open LibraryOL17097257M

      High‐resolution shock‐capturing schemes for inviscid and viscous hypersonic flows Yee, H.C.; Klopfer, G.H.; Montagné, J.L. Lower‐upper symmetric Gauss‐Seidel method for the Euler and Navier‐Stokes equations. Tenth International Conference on Numerical Methods in Fluid Dynamics Simulation of hypersonic viscous flows around a cone-delta-wing combination by an implicit method with multigrid acceleration. Numerical experiments with a symmetric high-resolution shock-capturing scheme.

    Numerical simulation of transient hypersonic flows involving shock-wave-freestream-disturbance interactions is presented using the essentially nonoscillatory (ENO) schemes. The EN0 schemes were chosen for transient-flow simulations because they have high-order accuracy at extrema as well as in other parts of smooth solutions. First, the. High-resolution shock-capturing schemes for inviscid and viscous hypersonic flows HC Yee, GH Klopfer, JL Montagne Journal of Computational Physics 88 (1), ,

    The full text of this article hosted at is unavailable due to technical difficulties. High-Resolution Shock Capturing Schemes for Inviscid and Viscous Hypersonic Flows," NASA TM , C. Park, and S Yoon, "Calculation of Real-Gas Effects on Blunt-Body Trim Angles," AIAA J., 30(4), (). A. Harten, "High Resolution Schemes for Hyperbolic Conservation Laws,'i l. of Computational Physics, 49, Author: 김규홍, 이경태, 김종암, 노오현.


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High-resolution shock-capturing schemes for inviscid and viscous hypersonic flows Download PDF EPUB FB2

JOURNAL OF COMPUTATIONAL PHYS () High-Resolution Shock-Capturing Schemes for Inviscid and Viscous Hypersonic Flows* H. YEE NASA Ames Research Center, Moffett Field, California G. KLOPFER NEAR Inc., Mountain View, California AND J.-L.

MONTAGNE1' ON ERA, B.P. 72, Chatillon Cedex, France Received Cited by: reviewed. A description of the two-parameter family implicit shock-capturing scheme, the various enhancements on numerical stability and convergence rate for hypersonic flows, and the behavior of the scheme for inviscid and viscous flows are discussed in the subsequent sections.

To illustrate the performance of the schemesCited by: HIGH-RESOLUTION SHOCK-CAPTURING SCHEMES FOR INVISCID AND VISCOUS HYPERSONIC FLOWS l B.C.

Yee 2 NASA Ames Research Center, Moffett Field, CA USA G.H. Klopfer 3 NEAR Inc., Mountain View, CA USA and J.-L. Montagn44 ONERA, B.P. 72, Chatillon Cedex, France Abstract i.

Get this from a library. High-resolution shock-capturing schemes for inviscid and viscous hypersonic flows. [H C Yee; Goetz H Klopfer; J -L Montagne; Ames Research Center.].

A class of high-resolution implicit total variation diminishing (TVD) type algorithms suitable for transonic multidimensional Euler and Navier-Stokes equations has been 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 Cited by: High-resolution shock-capturing schemes for inviscid and viscous hypersonic flows.

A class of high-resolution implicit total variation diminishing (TVD) type algorithms suitable for transonic multidimensional Euler and Navier-Stokes equations has been extended to hypersonic computations. The improved conservative shock-capturing schemes are spatially second- and.

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 : J.-L.

Montagne, G. Klopfer and H. Yee. High-resolution shock-capturing schemes for inviscid and viscous hypersonic flows. The development of robust, accurate, and efficient implicit shock-capturing schemes for multidimensional compressible Navier-Stokes equations in the hypersonic and real gas flow regimes is presently undertaken by extending a class of implicit total variation Author: J.-L.

Montagne, H. Yee and G. Klopfer. Jonas S., Messerschmid E., Frühauf H.H., Knab O. () Development and validation of a high resolution shock-capturing scheme for nonequilibrium hypersonic flows. In: Napolitano M., Sabetta F. (eds) Thirteenth International Conference on Numerical Methods in Fluid by: 6.

18 th Australasian Fluid Mechanics Conference Launceston, Australia December Applicability of Viscous and Inviscid Flow Solvers to the Hypersonic REST Inlet A.

Agon 1, D. Abeynayake 1 and M. Smart 2 1Defence Science and Technology Organisation Australia 2Centre for Hypersonics The University of Queensland, QueenslandAustraliaFile Size: KB. A class of high-resolution implicit total variation diminishing (TVD) type algorithms suitable for transonic multidimensional Euler and Navier-Stokes equations has been 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 Cited by: () High-resolution shock-capturing schemes for inviscid and viscous hypersonic flows.

Journal of Computational Physics() What does the entropy condition mean in traffic flow theory?.Cited by: The shock capturing method is employed to accurately compute double Mach reflection and viscous hypersonic flows over a circular half-cylinder and a.

Multidimensional High-Resolution Schemes for Viscous Hypersonic Flows. Bernard Parent; Bernard Parent. Pusan National University, BusanRepublic of Korea “ High-Resolution Shock-Capturing Schemes for Inviscid and Viscous Hypersonic Flows,” Journal of Computational Physics, Vol.

88, No. 1, Cited by: 2. Viscous Hypersonic Flow: Theory of Reacting and Hypersonic Boundary Layers (Dover Books on Engineering) [Dorrance, William H.] on *FREE* shipping on qualifying offers. Viscous Hypersonic Flow: Theory of Reacting and Hypersonic Boundary Layers (Dover Books on Engineering)4/5(2).

PDF | The first-order multidimensional flux difference splitting method (Parent, B., "Multidimensional Flux Difference Splitting Schemes," AIAA Journal, |. The first-order multidimensional flux difference splitting method (Parent, B., “Multidimensional Flux Difference Splitting Schemes,” AIAA Journal, Vol.

53, Cited by: 2. Those interested in problems of hypersonic inviscid flow and experimental techniques will not find those subjects covered in this book. Rather, it is intended that the various problems associated with a hot, reacting, compressible boundary layer will be thoroughly treated in the present book.

The Hypersonic Heating : Dover Publications. Numerica] issues for high-resolution shock-capturing schemes for inviscid and viscous hypersonic flows Description of the numerical algorithm A conservative linearized implicit form for unsteady and steady-state calculations General assumptions and limitations on the numerical studies File Size: 9MB.

Methods for the Accurate Computations of Hypersonic Flows: II. Shock-Aligned Grid Technique H. Yee, G. Kolpfer, and, J. Montague, High-Resolution Shock Capturing Schemes for Inviscid and Viscous Hypersonic Flows, NASA TMGoogle Scholar. 12Cited by:. A complex two-dimensional, unsteady, viscous hypersonic shock wave interaction is numerically simulated by a high-resolution, second-order fully implicit shock-capturing scheme.

The physical model consists of a non-stationary oblique shock impinging on the bow shock of a blunt by: 4.Thirteenth International Conference on Numerical Methods in Fluid Dynamics Development and validation of a high resolution shock-capturing scheme for nonequilibrium hypersonic flows.

Numerical simulation of inviscid and viscous flow with high order accurate schemes.H.C. Yee, Explicit and Implicit Compact High Resolution Shock-Capturing Methods for Multidimensional Euler Equations 1: Formulation, NASA Technical Report, TM ().

CPRF40 H.C. Yee, G.H. Klopfer, J.-L. Montagne, High resolution shock-capturing schemes for inviscid and viscous hypersonic flows, J. by: