Afbeelding 1 van 5
Afbeelding 1 van 5
Aircraft Engines and Gas Turbines by Kerrebrock. MIT Press, 1983
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“Very good book condition, good+ dust jacket condition: Dust jacket has some wrinkles and edge tears ”... Meer lezenover objectstaat
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Specificaties
- Objectstaat
- Heel goed
- Opmerkingen van verkoper
- Features
- Dust Jacket, Illustrated
- ISBN
- 9780262110648
- Book Title
- Aircraft Engines and Gas Turbines
- Publisher
- MIT Press
- Item Length
- 9 in
- Publication Year
- 1977
- Format
- Hardcover
- Language
- English
- Illustrator
- Yes
- Item Height
- 1 in
- Genre
- Transportation, Technology & Engineering
- Topic
- Aviation / General, Aeronautics & Astronautics
- Item Weight
- 24.7 Oz
- Item Width
- 6 in
- Number of Pages
- 248 Pages
Over dit product
Product Identifiers
Publisher
MIT Press
ISBN-10
0262110644
ISBN-13
9780262110648
eBay Product ID (ePID)
4443629
Product Key Features
Book Title
Aircraft Engines and Gas Turbines
Number of Pages
248 Pages
Language
English
Topic
Aviation / General, Aeronautics & Astronautics
Publication Year
1977
Illustrator
Yes
Genre
Transportation, Technology & Engineering
Format
Hardcover
Dimensions
Item Height
1 in
Item Weight
24.7 Oz
Item Length
9 in
Item Width
6 in
Additional Product Features
Intended Audience
Trade
LCCN
77-004428
Dewey Edition
19
Dewey Decimal
629.134'353
Synopsis
Aircraft Engines and Gas Turbines is widely used as a text in the United States and abroad, and has also become a standard reference for professionals in the aircraft engine industry., This text on aircraft engines and turbines presents the engine as a complete system, with emphasis on the performance of the engine and its dependence on the major design parameters and physical limitations. The system is described at three levels, first by ideal cycle and analysis, then by more refined cycle analysis, and finally as an assembly of components. At this last level the behavior of each component is described in terms of the fluid mechanical processes, chemistry, and mechanical stresses which limit its performance. The factors which control the engine's noise production and chemical pollutant emission are also addressed. Special emphasis is placed on the past, present and likely future evolution of the aircraft engine in response to the requirements for better performance, lower noise and reduced pollution. A clear appreciation of all these factors requires basic preparation in fluid mechanics, solid mechanics, chemistry and thermodynamics. Clearly, no single text can review all these: an undergraduate preparation is assumes. The application of these several disciplines to a complex system should help the students to appreciate their interrelationship as well as to understand the engine itself. With the rapid advances that have occurred since the large-scale introduction of gas turbine power plants into military aircraft in the 1950s and into commercial aircraft in the 1960s, it has become necessary to make a clear understanding of the characteristics of these devices accessible at the undergraduate level. Such understanding is essential both for entrance to professional work in industry and as preparation for graduate study. The book will also prove valuable as a reference for engineers already working in the field. Although the main focus is on aircraft propulsion, the text will also be useful to those interested in automotive and stationary applications of gas turbines. These applications are treated at the level of cycle analysis, and much of the discussion of components is directly applicable. The eleven chapters of the text take up basic definitions and concepts, trends in ideal cycle analysis, quantitative cycle analysis, nonrotating components, compressors, turbines, the structure of turbomachinery, component matching and engine performance, aircraft engine noise, hypersonic engines, and propulsion systems analysis. Each chapter includes problems and references., This text on aircraft engines and turbines presents the engine as a complete system, with emphasis on the performance of the engine and its dependence on the major design parameters and physical limitations.
LC Classification Number
TL709.5.T87
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