|
|
|
|
|
Leader |
LDR
|
|
pam i 00 |
|
Control # |
1
|
|
2017010103 |
|
Control # Id |
3
|
|
DLC |
|
Date |
5
|
|
20190911110925.0 |
|
Fixed Data |
8
|
|
170301s2017 enka b 001 0 eng |
|
LC Card |
10
|
|
$a 2017010103 |
|
ISBN |
20
|
|
$a9781292093093 (print) |
|
ISBN |
20
|
|
$z9781292093130 (pdf) |
|
ISBN |
20
|
|
$z9781292134482 (epub) |
|
Obsolete |
39
|
|
$a308939$cTLC |
|
Cat. Source |
40
|
|
$aDLC$beng$erda$cDLC$dGCG |
|
Authen. Ctr. |
42
|
|
$apcc |
|
LC Call |
50
|
00 |
$aTJ778$b.S24 2017 |
|
Dewey Class |
82
|
00 |
$a621.43/3$223 |
|
ME:Pers Name |
100
|
1 |
$aSaravanamuttoo, H. I. H.$eauthor. |
|
Title |
245
|
10 |
$aGas turbine theory /$cHIH Saravanamuttoo, professor emeritus, Department of Mechanical and Aerospace Engineering, Carleton University, GFC Rogers, Lately professor emeritus, University of Bristol, H Cohen, Lately fellow, Queens' College, Cambridge, PV Straznicky, professor emeritus, Department of Mechanical and Aerospace Engineering, Carleton University, AC Nix, assistant professor, Department of Mechanical and Aerospace Engineering, West Virginia University. |
|
Edition |
250
|
|
$a7th edition. |
|
Tag 264 |
264
|
1 |
$aHarlow, England ;$aNew York :$bPearson,$c2017. |
|
Phys Descrpt |
300
|
|
$axvii, 606 pages :$billustrations ;$c25 cm |
|
Tag 336 |
336
|
|
$atext$btxt$2rdacontent |
|
Tag 337 |
337
|
|
$aunmediated$bn$2rdamedia |
|
Tag 338 |
338
|
|
$avolume$bnc$2rdacarrier |
|
Note:Bibliog |
504
|
|
$aIncludes bibliographical references (pages 587-599) and index. |
|
Note:Content |
505
|
0 |
$a1. Introduction -- 1.1. Open-cycle single-shaft and twin-shaft arrangements -- 1.2. Multi-spool arrangements -- 1.3. Closed cycles -- 1.4. Aircraft propulsion -- 1.5. Industrial applications -- 1.6. Marine and land transportation -- 1.7. Environmental issues -- 1.8. Some future possibilities -- 1.9. Gas turbine design procedure -- 2. Shaft power cycles -- 2.1. Ideal cycles -- 2.2. Methods of accounting for component losses -- 2.3. Design point performance calculations -- 2.4. Comparative performance of practical cycles -- 2.5. Combined cycles and cogeneration schemes -- 2.6. Closed-cycle gas turbines -- 3. Gas turbine cycles for aircraft propulsion -- 3.1. Criteria of performance -- 3.2. Intake and propelling nozzle efficiencies -- 3.3. Simple turbojet cycle -- 3.4. The turbofan engine -- 3.5. The turboprop engine -- 3.6. The turboshaft engine -- 3.7. Auxiliary power units -- 3.8. Thrust augmentation -- 3.9. Miscellaneous topics -- 4. Centrifugal compressors -- 4.1. Principle of operation -- 4.2. Work done and pressure rise -- 4.3. The diffuser -- 4.4. Compressibility effects -- 4.5. Non-dimensional quantities for plotting compressor characteristics -- 4.6. Compressor characteristics -- 4.7. Computerized design procedures -- 5. Axial flow compressors -- 5.1. Basic operation -- 5.2. Elementary theory -- 5.3. Factors affecting stage pressure ratio -- 5.4. Blockage in the compressor annulus -- 5.5. Degree of reaction -- 5.6. Three-dimensional flow -- 5.7. Design process -- 5.8. Blade design -- 5.9. Calculation of stage performance -- 5.10. Compressibility effects -- 5.11. Off-design performance -- 5.12. Axial compressor characteristics -- 5.13. Closure -- 6. Combustion systems -- 6.1. Operational requirements -- 6.2. Types of combustion system -- 6.3. Some important factors affecting combustor design -- 6.4. The combustion process -- 6.5. Combustion chamber performance -- 6.6. Some practical problems -- 6.7. Gas turbine emissions -- 6.8. Pressure gain combustion -- 6.9. Coal gasification -- 7. Axial and radial flow turbines -- 7.1. Elementary theory of axial flow turbine -- 7.2. Vortex theory -- 7.3. Choice of blade profile, pitch and chord -- 7.4. Estimation of stage performance -- 7.5. Overall turbine performance -- 7.6. The cooled turbine -- 7.7. The radial flow turbine -- 8. Mechanical design of gas turbines -- 8.1. Design process -- 8.2. Gas turbine architecture -- 8.3. Loads and failure modes -- 8.4. Gas turbine materials -- 8.5. Design against failure and life estimations -- 8.6. Blades -- 8.7. Bladed rotor discs -- 8.8. Blade and disc vibration -- 8.9. Engine vibration -- 8.10. Power transmissions -- 8.12. Closure -- 9. Prediction of performance of simple gas turbines -- 9.1. Component characteristics -- 9.2. Off-design operation of the single-shaft gas turbine -- 9.3. Equilibrium running of a gas generator -- 9.4. Off-design operation of free turbine engine -- 9.5. Off-design operation of the jet engine -- 9.6. Methods of displacing the equilibrium running line -- 9.7. Incorporation of variable pressure losses -- 9.8. Power extraction -- 10. Prediction of performance, further topics -- 10.1. Methods of improving part load performance -- 10.2. Matching procedures for twin-spool engines -- 10.3. Some notes on the behaviour of twin-spool engines -- 10.4. Matching procedures for turbofan engines -- 10.5. Transient behaviours of gas turbines -- 10.6. Performance deterioration -- 10.7. Principles of control systems. |
|
Subj:Topical |
650
|
0 |
$aGas-turbines. |
|
AE:Pers Name |
700
|
1 |
$aRogers, G. F. C.$q(Gordon Frederick Crichton)$eauthor. |
|
AE:Pers Name |
700
|
1 |
$aCohen, Henry,$d1921 September 29-$eauthor. |
|
AE:Pers Name |
700
|
1 |
$aStraznicky, P. V,$eauthor. |
|
AE:Pers Name |
700
|
1 |
$aNix, A. C,$eauthor. |
