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Hypersonic Aerodynamics and Heat Transfer
Chapter 11: Heat Transfer and Flow Structure near the Planetary Probe Surface
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
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Chapter 11: Heat Transfer and Flow Structure near the Planetary Probe Surface
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Inhaltsverzeichnis
11.1: Introduction
11.2: Examined Configurations
11.3: Wind Tunnels and Flow Parameters
11.4: Heat Flux Probes
11.5: Method of Numerical Simulation of Laminar and Turbulent Flows
11.5.1 Formulation of the Problem
11.5.1.1 Differential Navier–Stokes Equations
11.5.1.2 Boundary and Initial Conditions
11.5.2 Reynolds-Averaged Navier–Stokes Equations
11.5.3 Modeling of Real Gas Flows
11.5.4 Approximation of Equations
11.5.5 Solution of Nonlinear Grid Equations
11.5.6 Solution of Systems of Linear Algebraic Equations
11.5.6.1 Direct Method of Solving a System of Linear Algebraic Equations
11.5.6.2 Iterative Method of Solving a System of Linear Algebraic Equations
11.5.6.3 Convergence Acceleration by Means of Preconditioning
11.5.7 Efficiency of the Numerical Solution of Grid Equations
11.5.8 Construction of the Computational Grid
11.5.9 Development of a Set of Universal Codes
11.5.10 Study of Convergence of the Calculated Data
11.6: Flow Structure and Heat Transfer near the Surface of Model No. 1
11.6.1 Laminar Flow
11.6.2 Transitional and Turbulent Flows
11.7: Flow Structure and Heat Transfer near the Surface of Model No. 2
11.7.1 Heat Transfer
11.7.2 Separation Region Length
11.8: Comparison of Models No. 1 and No. 2
11.9: Conclusions
Acknowledgments
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