An Introduction to Compressible Flow

Cover
Half Title
Title Page
Copyright Page
Table of Contents
Preface
Author Biographies
Chapter 1: Introduction
	1.1 Background Information on Gases
		1.1.1 Air Composition and Air Molecules
		1.1.2 Temperature and Gases
		1.1.3 Pressure and Gases
	1.2 Control Volume Analysis and Fundamental Concepts
		1.2.1 Basic Laws for a System
		1.2.2 Conservation of Mass
		1.2.3 Newton’s Second Law
		1.2.4 Energy Equation
		1.2.5 Development of a Generalized Control Volume Equation
		1.2.6 Conservation of Mass for a Control Volume
		1.2.7 Newton’s Second Law for a Control Volume
		1.2.8 Conservation of Energy for a Control Volume
		1.2.9 The Second Law of Thermodynamics for a Control Volume
	1.3 Review of Thermodynamics and the Ideal Gas Model
		1.3.1 Ideal Gas Law
		1.3.2 Specific Heats
		1.3.3 Tds Equations
	References
	Solved Problems
	Chapter 1 Problems
Chapter 2: Isentropic Flow
	2.1 Stagnation and Static Conditions
	2.2 The Speed of Sound in a Gas or Compressible Media
	2.3 One-Dimensional Isentropic Mach Number Relationships
	2.4 Converging Nozzles
	2.5 Flow in Varying Area Ducts
	2.6 Converging–Diverging Nozzles
	References
	Chapter 2 Problems
Chapter 3: Normal Shock Waves
	3.1 Subsonic and Supersonic Flow
	3.2 Normal Shock Wave Equations
		3.2.1 Reinforcement of Compression Waves into a Normal Shock Wave
		3.2.2 Normal Shock Wave Analysis
	3.3 Moving Shock Waves and Shock Reflections
	3.4 A Brief Introduction to Shock Tubes
	References
	Chapter 3 Problems
Chapter 4: Oblique Shock Waves
	4.1 Oblique Shock Wave Equations
		4.1.1 Analysis of an Oblique Shock Wave
	4.2 Supersonic Flow Over an Abrupt Wedge
	4.3 Supersonic Inlets, Nozzles, and Airfoils
		4.3.1 Oblique Shocks on Airfoils
	4.4 Oblique Shock Reflections
	4.5 Conical Shock Waves
	References
	Chapter 4 Problems
Chapter 5: An Introduction to Prandtl–Meyer Flow
	5.1 Prandtl–Meyer Expansion Fans
	5.2 Prandtl–Meyer Flow Equations
	5.3 Prandtl–Meyer Expansions
	5.4 Prandtl–Meyer Reflections
	5.5 Maximum Turning Angle for Prandtl–Meyer Flow
	References
	Chapter 5 Problems
Chapter 6: Applications
	6.1 Supersonic Wind Tunnel Startup
	6.2 Oblique Shock Diffusers
	6.3 Supersonic Airfoils
	6.4 Overexpanded and Underexpanded Supersonic Nozzles
	References
	Chapter 6 Problems
Chapter 7: Linearized Flow
	7.1 Introduction to Linearized Flow
	7.2 Development of the Linearized Pressure Coefficient
	7.3 Linearized Flow Over Airfoils
	7.4 Comparisons with the Shock Expansion Method
	References
	Chapter 7 Problems
Chapter 8: Internal Compressible Flow with Friction
	8.1 Introduction to Flow with Friction
	8.2 Analysis of the Fanno-Line and Interpretation of Flow Behavior
	8.3 Adiabatic Flow with Friction in a Constant Area Duct
	8.4 Application of Adiabatic Flow with Friction in a Constant Area Duct
	8.5 Isothermal Flow Assumption
	8.6 Adiabatic Flow with Friction and Area Change
	References
	Chapter 8 Problems
Chapter 9: Internal Compressible Flow with Heat Addition
	9.1 Introduction
	9.2 Constant Area Frictionless Flow with Heat Addition
	9.3 Rayleigh Line Analysis
	9.4 Frictionless Flow with Heat Addition and Area Change
	9.5 Constant Area Flow with Heat Transfer and Friction
	References
	Chapter 9 Problems
Appendix
	A.1 Isentropic Mach Number Tables
	A.2 Normal Shock Tables
Index
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