Classic and High-Enthalpy Hypersonic Flows

Classic and High-Enthalpy Hypersonic Flows

经典与高焓高超声速流动
基础力学

售价：

发货周期：国外库房发货,通常付款后3-5周到货！

作者

Joseph J.S. Shang

出版社

CRC Press

出版时间

2023年04月28日

装帧

精装

ＩＳＢＮ

9781032079813

复制

页码

310

开本

234 x 156 mm (6.14 x 9.21

语种

英文

版次

综合评分

暂无评分

图书详情
目次
买家须知
书评（0）
权威书评（0）

图书简介

Classic and High-Enthalpy Hypersonic Flows presents a complete look at high-enthalpy hypersonic flow from a review of classic theories to a discussion of future advances centering around the Born-Oppenheim approximation, potential energy surface, and critical point for transition. The state-of-the-art hypersonic flows are defined by a seamless integration of the classic gas dynamic kinetics with nonequilibrium chemical kinetics, quantum transitions, and radiative heat transfer. The book is intended for graduate students studying advanced aerodynamics and taking courses in hypersonic flow. It can also serve as a professional reference for practicing aerospace and mechanical engineers of high-speed aerospace vehicles and propulsion system research, design, and evaluation.FeaturesPresents a comprehensive review of classic hypersonic flow from the Newtonian theory to blast wave analogue.Introduces nonequilibrium chemical kinetics to gas dynamics for hypersonic flows in the high-enthalpy state.Integrates quantum mechanics to high-enthalpy hypersonic flows including dissociation and ionization. Covers the complete heat transfer process with radiative energy transfer for thermal protection of earth reentry vehicle.Develops and verifies the interdisciplinary governing equations for understanding and analyzing realistic hypersonic flows.

Part 1. Classic hypersonic flow theories. 1. Unique features of hypersonic flow fields. 1.1. General Remarks. 1.2. Free molecule, rarified, and continuum gas domains. 1.3. Mean free path. 1.4. Knudsen number. 1.5. Nonequilibrium chemical reactions. 1.6. Transport properties. 1.7. Internal degree of freedom. 1.8. Equation of state. Chapter 2. Aerodynamic governing equations. 2.1. Boltzmann equation. 2.2. Binary elastic collision. 2.3. Dynamic equilibrium state. 2.4. Maxwell distribution function. 2.5. Maxwell transfer and Euler equations. 2.6. Dynamic nonequilibrium state. 2.7. Navier-Stokes equation. 3. Inviscid flow. 3.1. Scope of inviscid flow domain. 3.2. Hypersonic similitudes. 3.3. Newtonian flow theory. 3.4. Rankine-Hugonoit relation. 3.5. Stand-off distance. 3.6. Mach number independent principle. 3.7. Tangent-wedge and Tangent-cone approximations. 3.8. Equivalence Principle or law of plane cross section. 3.9. Blast wave theory. 4. Viscous flow. 4.1. Compressible boundary-layer formulation. 4.2. Self-similar solutions. 4.3. Similarity numbers and parameters. 4.4. Stagnation-point heat transfer. 4.5. Laminar-turbulent transition. 4.6. Turbulent flow structure. 4.7. Compressible Turbulent Boundary layer. 4.8. Direct turbulence numerical simulation. 5. Viscous-inviscid interaction. 5.1. Computational simulations. 5.2. Leading edge Mach wave interaction. 5.3 Vorticity interaction. 5.4. Shock-boundary-layer interaction. 5.5. Three-dimensional corner flows. 5.6. Resonance and bifurcation. Part 2. High-enthalpy hypersonic flows. 6. Quantum transition. 6.1. Heisenberg uncertainty principle. 6.2. Quantum states of atom. 6.3. Quantum states of molecule. 6.4 Schrödinger equation. 6.5. Relaxation of quantum transition. 6.6. Conservation equations with quantum transition. 6.7. Quantum Jumps modeling. 6.8. Validating by flight data. 7. Statistic thermodynamics. 7.1. Microscopic state of gas mixture. 7.2. Thermodynamic equilibrium state. 7.3. Internal degrees of freedom.

Trade Policy 买家须知