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Gas Turbine Theory (6th Edition) By H.I.H. Saravanamuttoo
US $23.83
ApproximatelyS$ 30.65
Condition:
Very Good
A book that has been read but is in excellent condition. No obvious damage to the cover, with the dust jacket included for hard covers. No missing or damaged pages, no creases or tears, and no underlining/highlighting of text or writing in the margins. May be very minimal identifying marks on the inside cover. Very minimal wear and tear.
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Located in: MD, United States
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eBay item number:315256405028
Item specifics
- Condition
- Title
- Gas Turbine Theory (6th Edition)
- ISBN
- 9780132224376
- Book Title
- Gas Turbine Theory
- Publisher
- Prentice Hall PTR
- Item Length
- 9.3 in
- Edition
- 6
- Publication Year
- 2008
- Format
- Hardcover
- Language
- English
- Illustrator
- Yes
- Item Height
- 1.5 in
- Genre
- Technology & Engineering
- Topic
- Mechanical
- Item Weight
- 37.2 Oz
- Item Width
- 6.4 in
- Number of Pages
- 608 Pages
About this product
Product Identifiers
Publisher
Prentice Hall PTR
ISBN-10
0132224372
ISBN-13
9780132224376
eBay Product ID (ePID)
84569071
Product Key Features
Edition
6
Book Title
Gas Turbine Theory
Number of Pages
608 Pages
Language
English
Publication Year
2008
Topic
Mechanical
Illustrator
Yes
Genre
Technology & Engineering
Format
Hardcover
Dimensions
Item Height
1.5 in
Item Weight
37.2 Oz
Item Length
9.3 in
Item Width
6.4 in
Additional Product Features
LCCN
2008-027095
Dewey Edition
22
Dewey Decimal
621.433
Table Of Content
1 Introduction 2 Shaft power cycles 3 Gas turbine cyles for aircraft propulsion 4 Centrifugal compressors 5 Axial flow compressors 6 Combustion systems 7 Axial and radial flow turbines 8 Mechanical design of gas turbines 9 Prediction of performance of simple gas turbines 10 Prediction of performance - further topics Appendix A - Some notes on gas dynamics Appendix B - Problems Appendix C - references Index
Synopsis
Among the topics covered in this volume are: shaft power cycles; gas turbine cycles for aircraft propulsion; centrifugal compressors; axial flow compressors; combustion systems; axial and radial flow turbines; prediction of performance of simple gas turbines; and prediction of performance., In recent years the gas turbine, in combination with the steam turbine, has played an ever-increasing role in power generation. Despite the rapid advances in both output and efficiency, the basic theory of the gas turbine has remained unchanged. The layout of this new edition is broadly similar to the original, but greatly expanded and updated, comprising an outline of the basic theory, aerodynamic design of individual components, and the prediction of off-design performance. The addition of a chapter devoted to the mechanical design of gas turbines greatly enhances the scope of the book.
LC Classification Number
TJ778.S24 2008
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Value Added Tax Number:
- GB 724498118
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