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Название: Classic and High-Enthalpy Hypersonic Flows
Автор: Joseph J.S. Shang
Издательство: CRC Press
Год: 2023
Страниц: 327
Язык: английский
Формат: pdf (true)
Размер: 23.4 MB
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. Gas dynamic kinetics is the foundation for the physical description of all classic aerodynamic phenomena from subsonic, transonic, supersonic, to hypersonic flow domains.
Автор: Joseph J.S. Shang
Издательство: CRC Press
Год: 2023
Страниц: 327
Язык: английский
Формат: pdf (true)
Размер: 23.4 MB
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. Gas dynamic kinetics is the foundation for the physical description of all classic aerodynamic phenomena from subsonic, transonic, supersonic, to hypersonic flow domains.