Home Digitales Begell-Portal Begell eBook-Plattform Hypersonic Aerodynamics and Heat Transfer Chapter 16: Numerical Method of Solving Viscous Shock Layer Equations in a Wide Range of Reynolds Numbers

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 16: Numerical Method of Solving Viscous Shock Layer Equations in a Wide Range of Reynolds Numbers

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Inhaltsverzeichnis

16.1: Introduction

16.2: Formulation of the Problem

16.3: Characteristic Analysis of the System of VSL Equations and the Model of a Parabolic-Hyperbolic Viscous Shock Layer

16.4: Splitting of the Streamwise Pressure Gradient and Method of Global Iterations

16.5: Marching Method of Solving the Cauchy Problem with a Transonic Bifurcation

16.6: Convergence of Global Iterations

16.7: Conclusions

Acknowledgments

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