Titre : |
Gaz turbine engineering : applications, cycles and caracteristics |
Type de document : |
texte imprimé |
Auteurs : |
Richard T.C. Harman, Auteur |
Editeur : |
London : Macmillan |
Année de publication : |
1981 |
Importance : |
255 p. |
Présentation : |
ill. |
Format : |
25 cm |
ISBN/ISSN/EAN : |
978-0-333-30476-1 |
Note générale : |
Bibliogr. p. 256-263. Index |
Langues : |
Anglais (eng) |
Mots-clés : |
Mécanique. Turbine à gaz |
Index. décimale : |
621.438 Turbines de combustion.Turbines à gaz.Turbines à huile |
Résumé : |
This book appeal to final-year undergraduate students of mechanical engineering in universities and polytechnics. It will be of particular value to those taking a special option in gas turbines at the undergraduate or postgraduate level; it will also be useful on more broadly based design courses. The emphasis on practical contraining for young graduates. The contents of the book and each chapter progress in stages from an introductory to an adevanced level. Aircraft engine experience is used to discuss the design, operation, performance characteristics and current problems of radial and axial compressors and turbines, as well as combustion |
Note de contenu : |
Au sommaire :
- Applications for gas turbine engines
- Cycle calculation : design point performance
- Engine operation
- The centrifugal compressor
- The axial flow compressor
- Combustion
- The axial turbine
- The radial turbine
- Compressor operating characteristics
- Engine matching and transient characteristics
... |
Gaz turbine engineering : applications, cycles and caracteristics [texte imprimé] / Richard T.C. Harman, Auteur . - London : Macmillan, 1981 . - 255 p. : ill. ; 25 cm. ISBN : 978-0-333-30476-1 Bibliogr. p. 256-263. Index Langues : Anglais ( eng)
Mots-clés : |
Mécanique. Turbine à gaz |
Index. décimale : |
621.438 Turbines de combustion.Turbines à gaz.Turbines à huile |
Résumé : |
This book appeal to final-year undergraduate students of mechanical engineering in universities and polytechnics. It will be of particular value to those taking a special option in gas turbines at the undergraduate or postgraduate level; it will also be useful on more broadly based design courses. The emphasis on practical contraining for young graduates. The contents of the book and each chapter progress in stages from an introductory to an adevanced level. Aircraft engine experience is used to discuss the design, operation, performance characteristics and current problems of radial and axial compressors and turbines, as well as combustion |
Note de contenu : |
Au sommaire :
- Applications for gas turbine engines
- Cycle calculation : design point performance
- Engine operation
- The centrifugal compressor
- The axial flow compressor
- Combustion
- The axial turbine
- The radial turbine
- Compressor operating characteristics
- Engine matching and transient characteristics
... |
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