Numerical Simulation of Viscous Shock Layer Flows:
Gespeichert in:
1. Verfasser: | |
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Format: | Elektronisch E-Book |
Sprache: | English |
Veröffentlicht: |
Dordrecht
Springer Netherlands
1995
|
Schriftenreihe: | Fluid Mechanics and Its Applications
33 |
Schlagworte: | |
Online-Zugang: | Volltext |
Beschreibung: | The book is concerned with mathematical modelling of supersonic and hyper sonic flows about bodies. Permanent interest in this topic is stimulated, first of all, by aviation and aerospace engineering. The designing of aircraft and space vehicles requires a more precise prediction of the aerodynamic and heat transfer characteristics. Together with broadening of the flight condition range, this makes it necessary to take into account a number of gas dynamic and physical effects caused by rarefaction, viscous-inviscid interaction, separation, various physical and chemical processes induced by gas heating in the intensive bow shock wave. The flow field around a body moving at supersonic speed can be divided into three parts, namely, shock layer, near wake including base flow, and far wake. The shock layer flow is bounded by the bow shock wave and the front and lat eral parts of the body surface. A conventional approach to calculation of shock layer flows consists in a successive solution of the inviscid gas and boundary layer equations. When the afore-mentioned effects become important, implementation of these models meets difficulties or even becomes impossible. In this case, one has to use a more general approach based on the viscous shock layer concept |
Beschreibung: | 1 Online-Ressource (XII, 346 p) |
ISBN: | 9789401584906 9789048145942 |
ISSN: | 0926-5112 |
DOI: | 10.1007/978-94-015-8490-6 |
Internformat
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500 | |a The book is concerned with mathematical modelling of supersonic and hyper sonic flows about bodies. Permanent interest in this topic is stimulated, first of all, by aviation and aerospace engineering. The designing of aircraft and space vehicles requires a more precise prediction of the aerodynamic and heat transfer characteristics. Together with broadening of the flight condition range, this makes it necessary to take into account a number of gas dynamic and physical effects caused by rarefaction, viscous-inviscid interaction, separation, various physical and chemical processes induced by gas heating in the intensive bow shock wave. The flow field around a body moving at supersonic speed can be divided into three parts, namely, shock layer, near wake including base flow, and far wake. The shock layer flow is bounded by the bow shock wave and the front and lat eral parts of the body surface. A conventional approach to calculation of shock layer flows consists in a successive solution of the inviscid gas and boundary layer equations. When the afore-mentioned effects become important, implementation of these models meets difficulties or even becomes impossible. In this case, one has to use a more general approach based on the viscous shock layer concept | ||
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Datensatz im Suchindex
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any_adam_object | |
author | Golovachov, Yuri P. |
author_facet | Golovachov, Yuri P. |
author_role | aut |
author_sort | Golovachov, Yuri P. |
author_variant | y p g yp ypg |
building | Verbundindex |
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dewey-ones | 518 - Numerical analysis |
dewey-raw | 518 |
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dewey-sort | 3518 |
dewey-tens | 510 - Mathematics |
discipline | Mathematik |
doi_str_mv | 10.1007/978-94-015-8490-6 |
format | Electronic eBook |
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id | DE-604.BV042424064 |
illustrated | Not Illustrated |
indexdate | 2024-07-10T01:21:14Z |
institution | BVB |
isbn | 9789401584906 9789048145942 |
issn | 0926-5112 |
language | English |
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physical | 1 Online-Ressource (XII, 346 p) |
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publishDate | 1995 |
publishDateSearch | 1995 |
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publisher | Springer Netherlands |
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series2 | Fluid Mechanics and Its Applications |
spelling | Golovachov, Yuri P. Verfasser aut Numerical Simulation of Viscous Shock Layer Flows by Yuri P. Golovachov Dordrecht Springer Netherlands 1995 1 Online-Ressource (XII, 346 p) txt rdacontent c rdamedia cr rdacarrier Fluid Mechanics and Its Applications 33 0926-5112 The book is concerned with mathematical modelling of supersonic and hyper sonic flows about bodies. Permanent interest in this topic is stimulated, first of all, by aviation and aerospace engineering. The designing of aircraft and space vehicles requires a more precise prediction of the aerodynamic and heat transfer characteristics. Together with broadening of the flight condition range, this makes it necessary to take into account a number of gas dynamic and physical effects caused by rarefaction, viscous-inviscid interaction, separation, various physical and chemical processes induced by gas heating in the intensive bow shock wave. The flow field around a body moving at supersonic speed can be divided into three parts, namely, shock layer, near wake including base flow, and far wake. The shock layer flow is bounded by the bow shock wave and the front and lat eral parts of the body surface. A conventional approach to calculation of shock layer flows consists in a successive solution of the inviscid gas and boundary layer equations. When the afore-mentioned effects become important, implementation of these models meets difficulties or even becomes impossible. In this case, one has to use a more general approach based on the viscous shock layer concept Mathematics Computer science / Mathematics Mechanics Engineering mathematics Engineering Computational Mathematics and Numerical Analysis Mathematical Modeling and Industrial Mathematics Classical Continuum Physics Automotive Engineering Appl.Mathematics/Computational Methods of Engineering Informatik Ingenieurwissenschaften Mathematik https://doi.org/10.1007/978-94-015-8490-6 Verlag Volltext |
spellingShingle | Golovachov, Yuri P. Numerical Simulation of Viscous Shock Layer Flows Mathematics Computer science / Mathematics Mechanics Engineering mathematics Engineering Computational Mathematics and Numerical Analysis Mathematical Modeling and Industrial Mathematics Classical Continuum Physics Automotive Engineering Appl.Mathematics/Computational Methods of Engineering Informatik Ingenieurwissenschaften Mathematik |
title | Numerical Simulation of Viscous Shock Layer Flows |
title_auth | Numerical Simulation of Viscous Shock Layer Flows |
title_exact_search | Numerical Simulation of Viscous Shock Layer Flows |
title_full | Numerical Simulation of Viscous Shock Layer Flows by Yuri P. Golovachov |
title_fullStr | Numerical Simulation of Viscous Shock Layer Flows by Yuri P. Golovachov |
title_full_unstemmed | Numerical Simulation of Viscous Shock Layer Flows by Yuri P. Golovachov |
title_short | Numerical Simulation of Viscous Shock Layer Flows |
title_sort | numerical simulation of viscous shock layer flows |
topic | Mathematics Computer science / Mathematics Mechanics Engineering mathematics Engineering Computational Mathematics and Numerical Analysis Mathematical Modeling and Industrial Mathematics Classical Continuum Physics Automotive Engineering Appl.Mathematics/Computational Methods of Engineering Informatik Ingenieurwissenschaften Mathematik |
topic_facet | Mathematics Computer science / Mathematics Mechanics Engineering mathematics Engineering Computational Mathematics and Numerical Analysis Mathematical Modeling and Industrial Mathematics Classical Continuum Physics Automotive Engineering Appl.Mathematics/Computational Methods of Engineering Informatik Ingenieurwissenschaften Mathematik |
url | https://doi.org/10.1007/978-94-015-8490-6 |
work_keys_str_mv | AT golovachovyurip numericalsimulationofviscousshocklayerflows |