Difference Methods for Initial-Boundary-Value Problems and Flow Around Bodies

Difference Methods for Initial-Boundary-Value Problems and Flow Around Bodies PDF

Author: You-lan Zhu

Publisher: Springer Science & Business Media

Published: 2013-06-29

Total Pages: 606

ISBN-13: 3662067072

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Since the appearance of computers, numerical methods for discontinuous solutions of quasi-linear hyperbolic systems of partial differential equations have been among the most important research subjects in numerical analysis. The authors have developed a new difference method (named the singularity-separating method) for quasi-linear hyperbolic systems of partial differential equations. Its most important feature is that it possesses a high accuracy even for problems with singularities such as schocks, contact discontinuities, rarefaction waves and detonations. Besides the thorough description of the method itself, its mathematical foundation (stability-convergence theory of difference schemes for initial-boundary-value hyperbolic problems) and its application to supersonic flow around bodies are discussed. Further, the method of lines and its application to blunt body problems and conical flow problems are described in detail. This book should soon be an important working basis for both graduate students and researchers in the field of partial differential equations as well as in mathematical physics.

Hypersonic Inviscid Flow

Hypersonic Inviscid Flow PDF

Author: Wallace D. Hayes

Publisher: Courier Corporation

Published: 2012-07-13

Total Pages: 628

ISBN-13: 0486160483

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Unified, self-contained view of nonequilibrium effects, body geometries, and similitudes available in hypersonic flow and thin shock layer; appropriate for graduate-level courses in hypersonic flow theory. 1966 edition.

Scientific and Technical Aerospace Reports

Scientific and Technical Aerospace Reports PDF

Author:

Publisher:

Published: 1991

Total Pages: 1460

ISBN-13:

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Lists citations with abstracts for aerospace related reports obtained from world wide sources and announces documents that have recently been entered into the NASA Scientific and Technical Information Database.

Analysis of Three-dimensional Inviscid Supersonic Flow Between a Body and an Outer Wall

Analysis of Three-dimensional Inviscid Supersonic Flow Between a Body and an Outer Wall PDF

Author: W. C. Armstrong

Publisher:

Published: 1976

Total Pages: 98

ISBN-13:

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The three-dimensional inviscid supersonic flow equations are solved for the flow over a body located within a duct. Numerical solutions are obtained by use of the reference plane method of characteristics technique. Results of the analysis are compared with experimental test body pressure distributions obtained with an off-design jet stretcher system. The analysis is sufficiently general so that a variety of internal flows may be predicted. A computer program listing and an example problem are presented.