This book concentrates on modeling and numerical simulations of combustion in liquid rocket engines, covering liquid propellant atomization, evaporation of liquid droplets, turbulent flows, turbulent combustion, heat transfer, and combustion instability. It presents some state of the art models and numerical methodologies in this area. The book can be categorized into two parts. Part 1 describes the modeling for each subtopic of the combustion process in the liquid rocket engines. Part 2 presents detailed numerical methodology and several representative applications in simulations of rocket engine combustion.…mehr
This book concentrates on modeling and numerical simulations of combustion in liquid rocket engines, covering liquid propellant atomization, evaporation of liquid droplets, turbulent flows, turbulent combustion, heat transfer, and combustion instability. It presents some state of the art models and numerical methodologies in this area. The book can be categorized into two parts. Part 1 describes the modeling for each subtopic of the combustion process in the liquid rocket engines. Part 2 presents detailed numerical methodology and several representative applications in simulations of rocket engine combustion.Hinweis: Dieser Artikel kann nur an eine deutsche Lieferadresse ausgeliefert werden.
Zhen-Guo Wang, Professor & Head of Graduate School, National University of Defense Technology, Hunan, China Professor Wang has worked in the area of aeronautical and astronautical science and technology since the 1980s. This book is based on the teaching and supervision work of undergraduate and postgraduate students over the past 30 years. He is a Member of the Science and Technology Committee of the Ministry of Education, China, and Editor of Proceedings of the Institute of Mechanical Engineers, Part G: Journal of Aerospace Engineering. He has published two books (in Chinese) and over 100 peer-reviewed journal papers.
Inhaltsangabe
Preface x
1 Introduction 1
1.1 Basic Configuration of Liquid Rocket Engines 2
1.1.1 Propellant Feed System 2
1.1.2 Thrust Chamber 6
1.2 Internal Combustion Processes of Liquid Rocket Engines 13
1.2.1 Start and Shutdown 13
1.2.2 Combustion Process 15
1.2.3 Performance Parameters in Working Process 18
1.3 Characteristics and Development History of Numerical Simulation of the Combustion Process in Liquid Rocket Engines 19
1.3.1 Benefits of Numerical Simulation of the Combustion Process in Liquid Rocket Engines 19
1.3.2 Main Contents of Numerical Simulations of Liquid Rocket Engine Operating Process 19
1.3.3 Development of Numerical Simulations of Combustion Process in Liquid Rocket Engines 21
1.4 Governing Equations of Chemical Fluid Dynamics 22
1.5 Outline of this Book 24
References 25
2 Physical Mechanism and Numerical Modeling of Liquid Propellant Atomization 26
2.1 Types and Functions of Injectors in a Liquid Rocket Engine 27
2.2 Atomization Mechanism of Liquid Propellant 28
2.2.1 Formation of Static Liquid Droplet 28
2.2.2 Breakup of Cylindrical Liquid Jet 29
2.2.3 Liquid Sheet Breakup 36
2.2.4 Droplet Secondary Breakup 43
2.3 Characteristics of Atomization in Liquid Rocket Engines 48
2.3.1 Distribution Function of the Droplet Size 51
2.3.2 Mean Diameter and Characteristic Diameter 53
2.3.3 Measurement of Spray Size Distribution 55
2.4 Atomization Modeling for Liquid Rocket Engine Atomizers 59
2.4.1 Straight-flow Injector 60
2.4.2 Centrifugal Injector 60
2.4.3 Impinging-stream Injectors 64
2.4.4 Coaxial Shear Injector 70
2.4.5 Coaxial Centrifugal Injectors 70
2.5 Numerical Simulation of Liquid Propellant Atomization 75
2.5.1 Theoretical Models of Liquid Propellant Atomization 75
2.5.2 Quasi-fluid Models 80
2.5.3 Particle Trajectory Models 81
2.5.4 Simulation of Liquid Jet Atomization Using Interface Tracking Method 85
