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9780486419633

Elements of Gas Dynamics

by ;
  • ISBN13:

    9780486419633

  • ISBN10:

    0486419630

  • Format: Paperback
  • Copyright: 2002-01-11
  • Publisher: Dover Publications

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Summary

First-rate text covers introductory concepts from thermodynamics, one-dimensional gas dynamics and one-dimensional wave motion, waves in supersonic flow, flow in ducts and wind tunnels, methods of measurement, the equations of frictionless flow, small-perturbation theory, transonic flow, and much more. For advanced undergraduate or graduate physics and engineering students with at least a working knowledge of calculus and basic physics. Exercises demonstrate application of material in text.

Table of Contents

Concepts from Thermodynamics
Introduction
1(1)
Thermodynamic Systems
2(1)
Variables of State
3(1)
The First Principal Law
4(2)
Irreversible and Reversible Processes
6(1)
Perfect Gases
7(3)
The First Law Applied to Reversible Processes. Specific Heats
10(4)
The First Law Applied to Irreversible Processes
14(3)
The Concept of Entropy. The Second Law
17(3)
The Canonical Equation of State. Free Energy and Free Enthalpy
20(2)
Reciprocity Relations
22(1)
Entropy and Transport Processes
23(1)
Equilibrium Conditions
24(1)
Mixtures of Perfect Gases
25(2)
The Law of Mass Action
27(2)
Dissociation
29(4)
Condensation
33(1)
Real Gases in Gasdynamics
34(5)
One-Dimensional Gasdynamics
Introduction
39(1)
The Continuity Equation
40(1)
The Energy Equation
41(2)
Reservoir Conditions
43(2)
Euler's Equation
45(2)
The Momentum Equation
47(2)
Isentropic Conditions
49(1)
Speed of Sound; Mach Number
50(1)
The Area-Velocity Relation
51(2)
Results from the Energy Equation
53(2)
Bernoulli Equation; Dynamic Pressure
55(1)
Flow at Constant Area
56(1)
The Normal Shock Relations for a Perfect Gas
57(5)
One-Dimensional Wave Motion
Introduction
62(1)
The Propagating Shock Wave
62(3)
One-Dimensional Isentropic Equations
65(2)
The Acoustic Equations
67(1)
Propagation of Acoustic Waves
68(1)
The Speed of Sound
69(2)
Pressure and Particle Velocity in a Sound Wave
71(1)
``Linearized'' Shock Tube
72(2)
Isentropic Waves of Finite Amplitude
74(2)
Propagation of Finite Waves
76(2)
Centered Expansion Wave
78(1)
The Shock Tube
79(5)
Waves in Supersonic Flow
Introduction
84(1)
Oblique Shock Waves
85(1)
Relation between β and &thetas;
86(2)
Supersonic Flow over a Wedge
88(1)
Mach Lines
89(2)
Piston Analogy
91(1)
Weak Oblique Shocks
92(1)
Supersonic Compression by Turning
93(4)
Supersonic Expansion by Turning
97(1)
The Prandtl-Meyer Function
98(2)
Simple and Nonsimple Regions
100(1)
Reflection and Intersection of Oblique Shocks
101(1)
Intersection of Shocks of the Same Family
102(1)
Detached Shocks
103(3)
Mach Reflection
106(1)
Shock-Expansion Theory
107(2)
Thin Airfoil Theory
109(4)
Flat Lifting Wings
113(2)
Drag Reduction
115(3)
The Hodograph Plane
118(2)
Cone in Supersonic Flow
120(4)
Flow in Ducts and Wind Tunnels
Introduction
124(1)
Flow in Channel of Varying Area
124(1)
Area Relations
125(2)
Nozzle Flow
127(3)
Normal Shock Recovery
130(1)
Effects of Second Throat
131(2)
Actual Performance of Wind Tunnel Diffusers
133(1)
Wind Tunnel Pressure Ratio
133(3)
Supersonic Wind Tunnels
136(1)
Wind Tunnel Characteristics
137(2)
Compressor Matching
139(3)
Other Wind Tunnels and Testing Methods
142(2)
Methods of Measurement
Introduction
144(1)
Static Pressure
144(3)
Total Pressure
147(1)
Mach Number from Pressure Measurements
148(1)
Wedge and Cone Measurements
149(1)
Velocity
150(1)
Temperature and Heat Transfer Measurements
151(2)
Density Measurements
153(1)
Index of Refraction
153(4)
Schlieren System
157(2)
The Knife Edge
159(2)
Some Practical Considerations
161(1)
The Shadow Methods
162(2)
Interference Method
164(1)
Mach-Zehnder Interferometer
165(3)
Interferometer Techniques
168(2)
X-Ray Absorption and Other Methods
170(1)
Direct Measurement of Skin Friction
171(1)
Hot-Wire Probe
172(5)
Shock Tube Instrumentation
177(1)
The Equations of Frictionless Flow
Introduction
178(1)
Notation
178(2)
The Equation of Continuity
180(2)
The Momentum Equation
182(3)
The Energy Equation
185(1)
The Eulerian Derivative
186(2)
Splitting the Energy Equation
188(2)
The Total Enthalpy
190(1)
Natural Coordinates. Crocco's Theorem
191(3)
Relation of Vorticity to Circulation and Rotation
194(2)
The Velocity Potential
196(1)
Irrotational Flow
197(3)
Remarks on the Equations of Motion
200(2)
Small-Perturbation Theory
Introduction
202(1)
Derivation of the Pertubation Equations
203(3)
Pressure Coefficient
206(1)
Boundary Conditions
206(2)
Two-Dimensional Flow Past a Wave-Shaped Wall
208(4)
Wavy Wall in Supersonic Flow
212(3)
Supersonic Thin Airfoil Theory
215(1)
Planar Flows
216(2)
Bodies of Revolution. Slender Body Theory
Introduction
218(1)
Cylindrical Coordinates
219(2)
Boundary Conditions
221(3)
Pressure Coefficient
224(1)
Axially Symmetric Flow
224(2)
Subsonic Flow
226(1)
Supersonic Flow
226(3)
Velocities in the Supersonic Field
229(1)
Solution for a Cone
230(2)
Other Meridian Shapes
232(1)
Solution for Slender Cone
233(2)
Slender Body Drag
235(4)
Yawed Body of Revolution in Supersonic Flow
239(2)
Cross-Flow Boundary Conditions
241(1)
Cross-Flow Solutions
242(1)
Cross Flow for Slender Bodies of Revolution
242(1)
Lift of Slender Bodies of Revolution
243(3)
Slender Body Theory
246(1)
Rayleigh's Formula
247(5)
The Similarity Rules of High-Speed Flow
Introduction
252(1)
Two-Dimensional Linearized Flow. Prandtl-Glauert and Gothert Rules
253(3)
Two-Dimensional Transonic Flow. von Karman's Rules
256(2)
Linearized Axially Symmetric Flow
258(2)
Planar Flow
260(2)
Summary and Application of the Similarity Laws
262(1)
High Mach Numbers. Hypersonic Similarity
263(7)
Transonic Flow
Introduction
270(1)
Definition of the Transonic Range
270(1)
Transonic Flow Past Wedge Sections
271(5)
Transonic Flow Past a Cone
276(2)
Transonic Flow Past Smooth Two-Dimensional Shapes. The Question of Shock-Free Flow
278(2)
The Hodograph Transformation of the Equations
280(4)
The Method of Characteristics
Introduction
284(1)
Hyperbolic Equations
285(1)
The Compatibility Relation
285(3)
The Computation Method
288(3)
Interior and Boundary Points
291(1)
Axially Symmetric Flow
292(3)
Nonisentropic Flow
295(1)
Theorems about Plane Flow
296(2)
Computation with Weak, Finite Waves
298(1)
Interaction of Waves
299(2)
Design of Supersonic Nozzles
301(3)
Comparison of Characteristics and Waves
304(1)
Effects of Viscosity and Conductivity
Introduction
305(1)
Couette Flow
306(4)
Recovery Temperature
310(1)
Velocity Distribution in Couette Flow
311(2)
Rayleigh's Problem. The Diffusion of Vorticity
313(3)
The Bounary-Layer Concept
316(3)
Prandtl's Equations for a Flat Plate
319(1)
Characteristics Results from the Boundary-Layer Equation
320(3)
The Displacement Effect of the Boundary Layer. Momentum and Energy Integrals
323(2)
Change of Variables
325(1)
Boundary Layers on Profiles Other than a Flat Plate
326(3)
Flow through a Shock Wave
329(3)
The Navier-Stokes Equations
332(6)
The Turbulent Boundary Layer
338(2)
Boundary-Layer Effects on the External Flow Field
340(2)
Shock-Wave Boundary-Layer Interaction
342(4)
Turbulence
346(2)
Couette Flow of a Dissociating Gas
348(5)
Concepts from Gaskinetics
Introduction
353(2)
Probability Concepts
355(4)
Distribution Functions
359(2)
The Virial Theorem of Clausius
361(1)
The Equation of State of a Perfect Gas
362(1)
The Maxwell-Boltzmann Distribution
363(3)
The Specific Heats of Gases
366(3)
Molecular Collisions. Mean Free Path and Relaxation Times
369(3)
Shear Viscosity and Heat Conduction
372(1)
Couette Flow of a Highly Rarefied Gas
373(3)
The Concepts of Slip and Accommodation
376(2)
Relaxation Effects of the Internal Degrees of Freedom
378(2)
The Limit of Continuum Theory
380(3)
EXERCISES 383(20)
SELECTED REFERENCES 403(30)
TABLES
Critical Data and Characteristics Temperatures for Several Gases
405(1)
Flow Parameters versus M for Subsonic Flow
406(3)
Flow Parameters versus M for Supersonic Flow
409(9)
Parameters for Shock Flow
418(7)
Mach Number and Mach Angle versus Prandtl-Meyer Function
425(3)
CHARTS
Oblique Shock Chart
428(2)
Oblique Shock Chart
430(3)
Appendix 433(4)
Index 437

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