Fundamentals of compressible flow: with aircraft and rocket propulsion
Gespeichert in:
| 1. Verfasser: | |
|---|---|
| Format: | Buch |
| Sprache: | English |
| Veröffentlicht: |
Tunbridge Wells
New Age Science
2010
|
| Ausgabe: | 4. ed. |
| Schlagworte: | |
| Online-Zugang: | Inhaltsverzeichnis |
| Beschreibung: | XVII, 557 S. graph. Darst. |
| ISBN: | 9781906574321 1906574324 |
Internformat
MARC
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| 015 | |a GBA982500 |2 dnb | ||
| 020 | |a 9781906574321 |c hbk. : GBP 50.00 |9 978-1-906574-32-1 | ||
| 020 | |a 1906574324 |9 1-906574-32-4 | ||
| 035 | |a (OCoLC)501395704 | ||
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| 100 | 1 | |a Yahya, S. M. |e Verfasser |4 aut | |
| 245 | 1 | 0 | |a Fundamentals of compressible flow |b with aircraft and rocket propulsion |c S. M. Yahya |
| 250 | |a 4. ed. | ||
| 264 | 1 | |a Tunbridge Wells |b New Age Science |c 2010 | |
| 300 | |a XVII, 557 S. |b graph. Darst. | ||
| 336 | |b txt |2 rdacontent | ||
| 337 | |b n |2 rdamedia | ||
| 338 | |b nc |2 rdacarrier | ||
| 650 | 4 | |a Gas dynamics | |
| 650 | 4 | |a Compressibility | |
| 650 | 4 | |a Compressibility | |
| 650 | 4 | |a Gas dynamics | |
| 650 | 0 | 7 | |a Kompressible Strömung |0 (DE-588)4032018-2 |2 gnd |9 rswk-swf |
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| 999 | |a oai:aleph.bib-bvb.de:BVB01-018663458 | ||
Datensatz im Suchindex
| _version_ | 1804140751774285824 |
|---|---|
| adam_text | Contents
Preface
to the Fourth Edition
vii
Preface to the First Edition
ix
PART-I
1.
Definitions and Basic Relations
3-35
1.1
Fluid
3
1.2
System
3
1.3
Boundary
4
1.4
Control Volume
4
1.5
State
4
1.6
Process
4
1.7
Cycle
4
1.8
Property
4
1.9
Continuum
5
1.10
Pure Substance
5
1.11
Pressure
5
1.12
Density
5
1.13
Equilibrium
6
1.14
Temperature
6
1.15
Energy
6
1.16
Work
6
1.17
Heat
6
1.18
Zeroth Law of Thermodynamics
7
1.19
First Law of Thermodynamics
7
1.20
Specific Heats of Gases
8
1.21
Internal Energy and Enthalpy
9
1.22
Ideal Gas
9
xi
xii
Fundamentals of Compressible Flow
1.23
Equations of State 10
1.24
Real Gases n
1.25
Second Law of Thermodynamics
13
1.26
Reversible Flow 14
1.27
Irreversible Flow
14
1.28
Adiabatic Process
14
1.29
Change of Entropy 15
1.30
Third Law of Thermodynamics
15
1.31
Isentropic Process
15
1.32
Bulk Modulus of Elasticity
16
1.33
Coefficient of Compressibility
17
1.34
Fluid Velocity
17
1.35
Streamline
17
1.36
Stream Tube
17
1.37
Incompressible Flow
18
1.38
Compressible Flow
18
1.39
Steady Flow
18
1.40
Unsteady Flow
18
1.41
Flow Process
18
1.42
Non-flow Process
19
1.43
Viscosity
20
1.44
Reynolds Number
21
1.45 Mach
Number
21
1.46
Laminar Flow
22
1.47
Turbulent Flow
22
1.48
Coefficient of Skin Friction
22
1.49
Properties of the Atmosphere
25
2.
The Energy Equation
36-57
2.1
Energy Equation for a Non-flow Process
37
2.2
Energy Equation for a Flow Process
37
2.3
The Adiabatic Energy Equation
38
2.4
Stagnation Velocity of Sound
40
2.5
Stagnation Pressure
41
2.6
Stagnation Density
41
2.7
Stagnation State
41
2.8
Various Regions of Flow
42
2.9
Reference Velocities
43
2.10
Bernoulli Equation
47
2.11
Effect of
Mach
Number on Compressibility
49
Contents
xiii
3.
Rate Equations for a Control Volume
58-68
3.1
Continuity Equation (Conservation of Mass)
58
3.2
Momentum Equation (Conservation of Momentum)
60
3.3
Moment of Momentum Equation
61
3.4
Energy Equation (Conservation of Energy)
62
3.5
Entropy Equation
63
4.
Isentropic Flow with Variable Area
69-101
4.1
Comparison of Isentropic and Adiabatic Processes
69
4.2 Mach
Number Variation
72
4.3
Stagnation and Critical States
74
4.4
Area Ratio as Function of
Mach
Number
76
4.5
Impulse Function
78
4.6
Mass Flow Rate
79
4.7
Flow through Nozzles
84
4.8
Flow through Diffusers
88
4.9
Use of Gas Tables
89
5.
Wave Motion
102-133
5.1
Wave Propagation in an Elastic Solid Medium
102
5.2
Propagation of Infinitesimal Waves (Sound Waves)
103
5.3
Non-steep Finite Pressure Waves
112
5.4
Steep Finite Pressure Waves
115
5.5
Expansion Waves
121
6.
Flow with Normal Shock Waves
134-173
6.1
Development of a Shock Wave
134
6.2
Rarefaction Wave
135
6.3
The Governing Equations
136
6.4
Prandtl-Meyer Relation
139
6.5 Mach
Number Downstream of the Normal Shock Wave
141
6.6
Static Pressure Ratio Across the Shock
142
6.7
Temperature Ratio Across the Shock
143
6.8
Density Ratio Across the Shock (The Rankine-Hugoniot Equations)
144
6.9
Stagnation Pressure Ratio Across the Shock
146
6.10
Change in Entropy Across the Shock
147
6.11
Impossibility of a Shock in Subsonic Flow
148
6.12
Strength of a Shock Wave
149
6.13
Determination of
Mach
Number of Supersonic Flows
151
6.14
Tables and Charts for Normal Shock Waves
153
xiv
Fundamentals of Compressible Flow
6.15
Supersonic Wind Tunnels
153
6.16
Moving Normal Shock Waves
158
7.
Flow with Oblique Shock Waves
174-210
7.1
Nature of Flow through Oblique Shock Waves
176
7.2
Fundamental Relations
177
7.3
Prandtl s Equation
179
7.4
Rankine-Hugoniot Equation
181
7.5
Variation of Flow Parameters
182
7.6
Oblique Shock Relations from the Normal Shock Equations
188
7.7 Mach
Waves
188
7.8
Gas Tables for Oblique Shocks
189
7.9
Charts for Oblique Shocks
190
7.10
The Shock Polar Diagram
193
7.11
Expansion of Supersonic Flow
198
8.
Flow in Constant Area Ducts with Friction
211-246
8.1
The
Fanno
Curves
211
8.2
Fanno
Flow Equations
213
8.3
Solution of
Fanno
Flow Equations
216
8.4
Variation of Flow Properties
218
8.5
Variation of
Mach
Number with Duct Length
222
8.6
Tables for
Fanno
Flow
223
8.7
Charts for
Fanno
Flow
223
8.8
Isothermal Flow with Friction
224
9.
Flow in Constant Area Ducts wrm Heat Transfer
247-266
9.1
The Rayleigh Line
247
9.2
Fundamental Equations
251
9.3
Rayleigh Flow Relations
253
9.4
Variation of Flow Properties
256
9.5
Maximum Heat Transfer
257
9.6
Tables for Rayleigh Flow
258
9.7
Charts for Rayleigh Flow
259
PART-II
10.
Multi-dimensional Flow
269-301
10.1
Cartesian Coordinate System
269
10.2
Cylindrical Coordinate System
279
10.3
Potential Function
289
10.4
Stream Function
294
Contents
xv
11.
Methods of Measurement
302-354
11.1
Pressure
302
11.2
Temperature
308
11.3
Density
312
11.4
Velocity
312
11.5
Hot-wire Anemometer
315
11.6
Direction of Flow
318
11.7
Flow Rate
320
11.8
Wind Tunnels
328
11.9
Flow Visualization
336
11.10
Optical Methods
336
11.11
Laser Techniques
340
PART-III
12.
Aircraft Propulsion
357-395
12.1
Early Aircraft Engines
358
12.2
Types of Aircraft Engines
359
12.3
Aircraft Propulsion Theory
366
12.4
Ramjet Engine
380
12.5
Pulsejet
Engine
384
13.
Rocket Propulsion
396-459
13.1
Early Rocket Engines
397
13.2
Types of Rocket Engines
398
13.3
Liquid Propellant Rocket Engines
404
13.4
Solid Propellant Rocket Motors
414
13.5
Rocket Propulsion Theory
421
13.6
Rocket Applications
431
13.7
Space Flights
434
14.
Miscellaneous Problems in Compressible Flow
460-513
14.1
Falkner s Friction Factor
460
14.2
Height above Sea Level for given Atmospheric Temperature
and Pressure
461
14.3
Differential Form of Equation of Continuity
461
14.4
Air-Jet Velocity Temperature Equal to Twice its Static
Temperature
462
14.5
Flow Rate, Power Required and Pressure Developed in
a Centrifugal Fan
463
14.6
Variation of Cross-sectional Area with
Mach
Number
for Isentropic Flow
465
xvi
Fundamentals of Compressible Flow
14.7
Stagnation Pressure for Maximum Mass Flow Rate in a
Convergent-divergent Nozzle
466
14.8
Compressible Flow (from
M
= 0.2
to
0.9)
in an Accelerating Duct
467
14.9
Isentropic Flow in a Supersonic
Diffuser
468
14.10
Velocities of Infinitesimal Pressure Waves in Water and Steel
469
14.11
Velocity of Sound in
Freon
469
14.12
Mach
Number Upstream of a Normal Shock
469
14.13
Traversing of Non-steep Finite Pressure Wave and Steep Pressure
Wave through Stagnant Air
470
14.14
Supersonic
Diffuser
with a Normal Shock
471
14.15
Supersonic Flow Over Corners of a Convex Wall
473
14.16
Supersonic Flow Over a Concave Wall
474
14.17
Flow with Friction in a Long Duct Upstream of a
Convergent-divergent Nozzle
476
14.18
Flow with Friction in a Long Duct Downstream of a
Supersonic Nozzle
478
14.19
Flow with Friction in a Long Pipe between a Convergent
Nozzle and an Exhauster
480
14.20
Flow Through a Variable Exit Area Convergent Nozzle
482
14.21
Supersonic Flow through a Combustion Chamber with and
without a Shock
485
14.22
Heating of Air at Subsonic and Supersonic
Mach
Numbers
to Maximum Stagnation Temperature
487
14.23
Discharge of High Pressure Air from a Settling Chamber
through a Circular Pipe
489
14.24
Calculation of Velocity of Air from Measured Value of the
Dynamic Head
490
14.25
Static Pressure Rise through the
Diffuser
and Compressor
of a Turboprop Engine
491
14.26
Fuel-Air Ratio, Compressor and Turbine and Exhaust Nozzle
Pressure Ratio of a Turbojet Engine
493
14.27
Isothermal Flow in a Constant Area Duct with Friction
495
14.28
Isothermal Flow of Gas
(γ
= 1.26)
through Pipe-Lines
between the Pumping Stations
496
14.29
Radial Pressure Gradient in Radial Equilibrium Flow
501
14.30
Steady and Inviscid Flow in Radial Equilibrium
502
14.31
Change in Stagnation Pressure in Unsteady Flow
503
14.32
Energy Transfer in Unsteady Flow
503
14.33
Potential Function Equation for Unsteady Flow
504
14.34
Continuity Equation for Unsteady Flow
505
14.35
Moving Shock Wave
505
14.36
Subsonic Wind Tunnels
506
14.37
Isothermal Flow with Variable Area
508
Contents
xvii
14.38
Pressure and Density Ratios for Low
Mach
Numbers
509
14.39
Actual
Mach
Number and Velocity at Nozzle Exit
510
14.40
Frictionless Flow with Heat Transfer
511
Appendices
517-545
Bibliography
547-549
Index
551-557
|
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| id | DE-604.BV035804386 |
| illustrated | Illustrated |
| indexdate | 2024-07-09T22:04:58Z |
| institution | BVB |
| isbn | 9781906574321 1906574324 |
| language | English |
| oai_aleph_id | oai:aleph.bib-bvb.de:BVB01-018663458 |
| oclc_num | 501395704 |
| open_access_boolean | |
| owner | DE-703 DE-634 |
| owner_facet | DE-703 DE-634 |
| physical | XVII, 557 S. graph. Darst. |
| publishDate | 2010 |
| publishDateSearch | 2010 |
| publishDateSort | 2010 |
| publisher | New Age Science |
| record_format | marc |
| spelling | Yahya, S. M. Verfasser aut Fundamentals of compressible flow with aircraft and rocket propulsion S. M. Yahya 4. ed. Tunbridge Wells New Age Science 2010 XVII, 557 S. graph. Darst. txt rdacontent n rdamedia nc rdacarrier Gas dynamics Compressibility Kompressible Strömung (DE-588)4032018-2 gnd rswk-swf Kompressible Strömung (DE-588)4032018-2 s DE-604 Digitalisierung UB Bayreuth application/pdf http://bvbr.bib-bvb.de:8991/F?func=service&doc_library=BVB01&local_base=BVB01&doc_number=018663458&sequence=000002&line_number=0001&func_code=DB_RECORDS&service_type=MEDIA Inhaltsverzeichnis |
| spellingShingle | Yahya, S. M. Fundamentals of compressible flow with aircraft and rocket propulsion Gas dynamics Compressibility Kompressible Strömung (DE-588)4032018-2 gnd |
| subject_GND | (DE-588)4032018-2 |
| title | Fundamentals of compressible flow with aircraft and rocket propulsion |
| title_auth | Fundamentals of compressible flow with aircraft and rocket propulsion |
| title_exact_search | Fundamentals of compressible flow with aircraft and rocket propulsion |
| title_full | Fundamentals of compressible flow with aircraft and rocket propulsion S. M. Yahya |
| title_fullStr | Fundamentals of compressible flow with aircraft and rocket propulsion S. M. Yahya |
| title_full_unstemmed | Fundamentals of compressible flow with aircraft and rocket propulsion S. M. Yahya |
| title_short | Fundamentals of compressible flow |
| title_sort | fundamentals of compressible flow with aircraft and rocket propulsion |
| title_sub | with aircraft and rocket propulsion |
| topic | Gas dynamics Compressibility Kompressible Strömung (DE-588)4032018-2 gnd |
| topic_facet | Gas dynamics Compressibility Kompressible Strömung |
| url | http://bvbr.bib-bvb.de:8991/F?func=service&doc_library=BVB01&local_base=BVB01&doc_number=018663458&sequence=000002&line_number=0001&func_code=DB_RECORDS&service_type=MEDIA |
| work_keys_str_mv | AT yahyasm fundamentalsofcompressibleflowwithaircraftandrocketpropulsion |