LIQUID ROCKET ENGINE : THRUST CHAMBER PARAMETRIC MODELING

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Detalles Bibliográficos
Clasificación:Libro Electrónico
Autor principal: Rezende, Rene Nardi (Autor)
Formato: Electrónico eBook
Idioma:Inglés
Publicado: WARRENDALE : SAE SOC OF AUTOMOTIVE ENG, 2018.
Temas:
Liquid propellant rocket engines.
Acceso en línea:Texto completo
Tabla de Contenidos:
  • Cover
  • Table of contents
  • Acknowledgments
  • Nomenclature
  • CHAPTER 1 Introduction
  • 1.1 Background
  • 1.2 Work Objectives
  • 1.3 Scope of the Work
  • 1.4 Comments on the Project Life Cycle
  • 1.5 Parametric Modeling Basics
  • References
  • CHAPTER 2 Fundamentals of Rocket Propulsion
  • 2.1 Introduction
  • 2.2 The Main References: A Historical Perspective
  • 2.3 Parametric Modeling Application Review
  • 2.4 What Is Jet Propulsion?
  • 2.5 The de Laval Nozzle
  • 2.6 Thrust Equation
  • 2.7 Standard Atmosphere
  • References
  • CHAPTER 3 Methodology
  • 3.1 Project Flowchart
  • 3.2 High-Level Requirements
  • 3.3 Combustion Gases Properties
  • 3.3.1 Mixture Ratio
  • 3.3.2 Adiabatic Flame Temperature
  • 3.3.3 Molar Mass
  • 3.3.4 Specific Heats Ratio
  • 3.3.5 Sources of Data
  • 3.4 Propellant Properties
  • 3.4.1 Fuels
  • 3.4.2 Oxidizers
  • References
  • CHAPTER 4 Thrust Chamber Performance Assessment
  • 4.1 A Parameter for Thrust Chamber Performance Assessment
  • 4.2 Conditions for an Ideal Thrust Chamber
  • 4.3 Theoretical Performance
  • 4.4 Correction Factors
  • 4.5 Validations
  • References
  • CHAPTER 5 Nozzle Dimensioning
  • 5.1 Throat Section Dimensioning
  • 5.1.1 Throat Section Dimensioning: First Method
  • 5.1.2 Throat Section Dimensioning: Second Method
  • 5.2 Exhaust Section Dimensioning
  • 5.2.1 Exhaust Section Dimensioning: First Method
  • 5.2.2 Exhaust Section Dimensioning: Second Method
  • 5.3 When Nozzle Operates Out of the Optimal Point
  • 5.4 Validations
  • References
  • CHAPTER 6 Combustion Chamber Dimensioning
  • 6.1 Introduction
  • 6.2 Combustion Chamber Volume
  • 6.3 Combustion Chamber Diameter
  • 6.4 Combustion Chamber Length
  • 6.5 Chamber Wall Thickness
  • 6.6 Model Assessment
  • 6.7 Validations
  • References
  • CHAPTER 7 Nozzle Configuration
  • 7.1 Introduction
  • 7.2 Conical Nozzle
  • 7.3 Parabolic Nozzle
  • 7.4 Validation
  • References
  • CHAPTER 8 Complementing the Performance Calculation
  • 8.1 Propellant Consumption
  • 8.2 Nozzle Flow Equations
  • 8.3 Validations
  • References
  • CHAPTER 9 The Cold Section
  • 9.1 Introduction
  • 9.2 Impinging Jets
  • 9.3 Shower Head
  • 9.4 Swirl, Pressure Swirl, or Spray
  • 9.5 Pintle
  • References
  • CHAPTER 10 The Simplex Swirl Injector
  • 10.1 Introduction
  • 10.2 Swirl Injection Operation
  • 10.3 Problem Statement
  • 10.4 The Outlet Orifice
  • 10.5 The Inlet Orifices
  • 10.6 Sizing Methodology
  • 10.7 Validation
  • References
  • CHAPTER 11 The Pintle Injector
  • 11.1 Introduction
  • 11.2 General Characteristics
  • 11.3 Qualitative Analyses: Flow Visualization
  • 11.4 Quantitative Analyses: Design Parameters
  • 11.5 Validation
  • 11.5.1 The 1000-N Injector
  • 11.5.2 Validation: The 5000-N Injector
  • References
  • CHAPTER 12 Appendix
  • 12.1 Ground Test
  • 12.1.1 Testing a Complete Engine
  • Hot Test
  • 12.1.2 Testing the Propellant Injector
  • Cold Test
  • 12.2 Propellants Charts
  • 12.2.1 Liquid Oxygen and Ethanol

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