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Fundamentals of Gas Dynamics 2nd edition [Kõva köide]

  • Formaat: Hardback, 280 pages, kõrgus x laius x paksus: 254x178x19 mm, kaal: 1361 g
  • Ilmumisaeg: 22-Dec-2014
  • Kirjastus: John Wiley & Sons Inc
  • ISBN-10: 1118973399
  • ISBN-13: 9781118973394
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Fundamentals of Gas Dynamics 2nd editionSuurem pilt
  • Formaat: Hardback, 280 pages, kõrgus x laius x paksus: 254x178x19 mm, kaal: 1361 g
  • Ilmumisaeg: 22-Dec-2014
  • Kirjastus: John Wiley & Sons Inc
  • ISBN-10: 1118973399
  • ISBN-13: 9781118973394
Teised raamatud teemal:
Püsilink: https://www.kriso.ee/db/9781118973394.html

Fundamentals of Gas Dynamics, Second Edition isa comprehensively updated new edition and now includes a chapter on the gas dynamics of steam. It covers the fundamental concepts and governing equations of different flows, and includes end of chapter exercises based on the practical applications. A number of useful tables on the thermodynamic properties of steam are also included.

Fundamentals of Gas Dynamics, Second Edition begins with an introduction to compressible and incompressible flows before covering the fundamentals of one dimensional flows and normal shock waves. Flows with heat addition and friction are then covered, and quasi one dimensional flows and oblique shock waves are discussed. Finally the prandtl meyer flow and the flow of steam through nozzles are considered.

Preface vii
1 Introduction
1(8)
1.1 Compressibility of Fluids
1(1)
1.2 Compressible and Incompressible Flows
2(1)
1.3 Perfect Gas Equation of State
3(3)
1.3.1 Continuum Hypothesis
4(2)
1.4 Calorically Perfect Gas
6(3)
2 One Dimensional Flows - Basics
9(16)
2.1 Governing Equations
9(2)
2.2 Acoustic Wave Propagation Speed
11(3)
2.2.1 Mach Number
13(1)
2.3 Reference States
14(5)
2.3.1 Sonic State
14(1)
2.3.2 Stagnation State
14(5)
2.4 T-s and P-v Diagrams in Compressible Flows
19(6)
Exercises
23(2)
3 Normal Shock Waves
25(14)
3.1 Governing Equations
25(2)
3.2 Mathematical Derivation of the Normal Shock Solution
27(5)
3.3 Illustration of the Normal Shock Solution on T-s and P-v diagrams
32(2)
3.4 Further Insights into the Normal Shock Wave Solution
34(5)
Exercises
37(2)
4 Flow with Heat Addition- Rayleigh Flow
39(18)
4.1 Governing Equations
39(1)
4.2 Illustration on T-s and P-v diagrams
40(8)
4.3 Thermal Choking and Its Consequences
48(4)
4.4 Calculation Procedure
52(5)
Exercises
55(2)
5 Flow with Friction - Fanno Flow
57(12)
5.1 Governing Equations
58(1)
5.2 Illustration on T-s diagram
58(4)
5.3 Friction Choking and Its Consequences
62(1)
5.4 Calculation Procedure
62(7)
Exercises
67(2)
6 Quasi One Dimensional Flows
69(38)
6.1 Governing Equations
70(1)
6.1.1 Impulse Function and Thrust
70(1)
6.2 Area Velocity Relation
71(2)
6.3 Geometric Choking
73(2)
6.4 Area Mach number Relation for Choked Flow
75(1)
6.5 Mass Flow Rate for Choked Flow
76(1)
6.6 Flow Through A Convergent Nozzle
77(5)
6.7 Flow Through A Convergent Divergent Nozzle
82(10)
6.8 Interaction between Nozzle Flow and Fanno, Rayleigh Flows
92(15)
Exercises
102(5)
7 Oblique Shock Waves
107(18)
7.1 Governing Equations
109(2)
7.2 θ-β-M curve
111(2)
7.3 Illustration of the Weak Oblique Shock Solution on a T-s diagram
113(6)
7.4 Detached Shocks
119(2)
7.5 Reflected Shocks
121(4)
7.5.1 Reflection from a Wall
121(2)
Exercises
123(2)
8 Prandtl Meyer Flow
125(14)
8.1 Propagation of Sound Waves and the Mach Wave
126(3)
8.2 Prandtl Meyer Flow Around Concave and Convex Corners
129(2)
8.3 Prandtl Meyer Solution
131(4)
8.4 Reflection of Oblique Shock From a Constant Pressure Boundary
135(4)
Exercises
137(2)
9 Flow of Steam through Nozzles
139(88)
9.1 T-s diagram of liquid water-water vapor mixture
141(1)
9.2 Isentropic expansion of steam
142(3)
9.3 Flow of steam through nozzles
145(7)
9.3.1 Choking in steam nozzles
146(6)
9.4 Supersaturation and the condensation shock
152(11)
Exercises
159(4)
A Isentropic table for γ = 1.4
163(10)
B Normal shock properties for γ = 1.4
173(8)
C Rayleigh flow properties for γ = 1.4
181(10)
D Fanno flow properties for γ = 1.4
191(10)
E Oblique shock wave angle β in degrees for γ = 1.4
201(6)
F Mach angle and Prandtl Meyer angle for γ = 1.4
207(4)
G Thermodynamic properties of steam, temperature table
211(4)
H Thermodynamic properties of steam, pressure table
215(4)
I Thermodynamic properties of superheated steam
219(8)
Index 227
V. Babu, IIT Madras, India Dr. V. Babu is an Associate Professor in the Department of Mechanical Engineering at IIT Madras. His primary research specialization is CFD and he is currently involved in the simulation of high speed reacting flows, prediction of jet noise, simulation of fluid flows using the lattice Boltzmann method and high performance computing. In 1998 he received the Henry Ford Technology Award for the development and deployment of a virtual wind tunnel. He also has four US patents to his credit.