Home Digitales Begell-Portal Begell eBook-Plattform Hypersonic Aerodynamics and Heat Transfer Chapter 13: Numerical Modeling of Hypersonic Heat Transfer on the Windward Side of the Buran Reentry Vehicle

Hypersonic Aerodynamics and Heat Transfer

ISBN Druckformat: 978-1-56700-309-3

ISBN Online: 978-1-56700-287-4

Sergey Vladimirovich Utyuzhnikov The University of Manchester, Oxford Road, Manchester M13 9PL, United Kingdom

G. A. Tirskiy Moscow Institute for Physics and Technology, Moscow, Russia

Chapter 13: Numerical Modeling of Hypersonic Heat Transfer on the Windward Side of the Buran Reentry Vehicle

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Inhaltsverzeichnis

13.1: Introduction

13.2: Model of the Medium

13.3: Constitutive Equations and Method of Solving the Problem

13.4: Calculation of the Flow around the Buran Reentry Vehicle

13.5: Conclusions

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