Basics of Aerothermodynamics

Ernst Heinrich Hirschel

412 pages, parution le 14/10/2004

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Résumé

The basics of aerothermodynamics are treated in this book with special regard to the fact that outer surfaces of hypersonic vehicles primarily are radiation cooled. The implications of this fact are different for different vehicle classes. In any case the properties of both attached viscous and separated flows are of importance in this regard. After a discussion of flight environment and transport phenomena in general, the most important aerothermodynamic phenomena are treated. Thermal surface effects are particularly considered, taking into account both radiation cooling and/or active cooling, for example of inner surfaces. Finally the simulation means of aerothermodynamics are discussed. Computational methods and their modelling problems as well as the problems of ground facility and flight simulation, including the hot experimental technique, are treated.

Written for: Engineers and scientists in aerothermodynamics

Sommaire

Introduction
The Flight Environment
The Thermal State of the Surface
Transport of Momentum, Energy and Mass
Real-Gas Aerothermodynamic Phenomena
Inviscid Aerothermodynamic Phenomena
Attached High-Speed Viscous Flow
Laminar-Turbulent Transition and Turbulence in High-Speed Viscous Flow
Strong Interaction Phenomena
Simulation Means
The RHPM-Flyer
Governing Equations for Flow in General Coordinates
Constants, Functions, Dimensions and Conversions
Symbols

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	PAPIER
Éditeur(s)	Springer
Auteur(s)	Ernst Heinrich Hirschel
Parution	14/10/2004
Nb. de pages	412
Format	16 x 24
Couverture	Relié
Poids	846g
Intérieur	Noir et Blanc
EAN13	9783540221326
ISBN13	978-3-540-22132-6