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Fundamentals of jet propulsion with applications / Ronald D Flack 

Public ISBD Titre : Fundamentals of jet propulsion with applications Type de document : texte imprimé Auteurs : Ronald D Flack, Auteur Editeur : Cambridge : Cambridge University Press Année de publication : 2005 Collection : Cambridge Aerospace Series Importance : 658 p. Présentation : ill. Format : 26 cm ISBN/ISSN/EAN : 978-0-521-81983-1 Note générale : Bibliogr. p.623-627. Index Langues : Anglais (eng) Mots-clés : Compresseurs  --  Compresseurs  supersoniques Turbines  --  Turbines  à  gaz Turbogénérateurs Avions  --  Turboréacteurs Propulsion  par  réaction  --  Aéronautique Moteurs  à  réaction  --  Avions  à  réaction Index. décimale : 62-843 Moteurs à combustion interne Résumé : This introductory text on air-breathing jet propulsion focuses on the basic operating principles of jet engines and gas turbines. Previous coursework in fluid mechanics and thermodynamics is elucidated and applied to help the student understand and predict the characteristics of engine components and various types of engines and power gas turbines. Numerous examples help the reader appreciate the methods and differing, representative physical parameters. A capstone chapter integrates the text material in a portion of the book devoted to system matching and analysis so that engine performance can be predicted for both on- and off-design conditions. The book is designed for advanced undergraduate and first-year graduate students in aerospace and mechanical engineering. A basic understanding of fluid dynamics and thermodynamics is presumed. Although aircraft propulsion is the focus, the material can also be used to study ground- and marine-based gas turbines and turbomachinery and some advanced topics in compressors and turbines. Note de contenu : * Cycle Analysis - Ideal cycle analysis - Non-ideal cycle analysis * Component Analysis - Diffusers - Nozzles - Axial flow compressors and fans - Centrifugal compressors - Axial flow turbines - Combustors and afterburners - Ducts and mixers * System Matching and Analysis - Matching of gas turbine components En ligne : http://www.amazon.fr/gp/redirect.html%3FASIN=0521819830%26tag=ws%26lcode=xm2%26c [...] Fundamentals of jet propulsion with applications [texte imprimé] / Ronald D Flack, Auteur . - Cambridge University Press, 2005 . - 658 p. : ill. ; 26 cm. - (Cambridge Aerospace Series) . ISBN : 978-0-521-81983-1 Bibliogr. p.623-627. Index Langues : Anglais (eng) Mots-clés : Compresseurs  --  Compresseurs  supersoniques Turbines  --  Turbines  à  gaz Turbogénérateurs Avions  --  Turboréacteurs Propulsion  par  réaction  --  Aéronautique Moteurs  à  réaction  --  Avions  à  réaction Index. décimale : 62-843 Moteurs à combustion interne Résumé : This introductory text on air-breathing jet propulsion focuses on the basic operating principles of jet engines and gas turbines. Previous coursework in fluid mechanics and thermodynamics is elucidated and applied to help the student understand and predict the characteristics of engine components and various types of engines and power gas turbines. Numerous examples help the reader appreciate the methods and differing, representative physical parameters. A capstone chapter integrates the text material in a portion of the book devoted to system matching and analysis so that engine performance can be predicted for both on- and off-design conditions. The book is designed for advanced undergraduate and first-year graduate students in aerospace and mechanical engineering. A basic understanding of fluid dynamics and thermodynamics is presumed. Although aircraft propulsion is the focus, the material can also be used to study ground- and marine-based gas turbines and turbomachinery and some advanced topics in compressors and turbines. Note de contenu : * Cycle Analysis - Ideal cycle analysis - Non-ideal cycle analysis * Component Analysis - Diffusers - Nozzles - Axial flow compressors and fans - Centrifugal compressors - Axial flow turbines - Combustors and afterburners - Ducts and mixers * System Matching and Analysis - Matching of gas turbine components En ligne : http://www.amazon.fr/gp/redirect.html%3FASIN=0521819830%26tag=ws%26lcode=xm2%26c [...]

Exemplaires

Code-barres	Cote	Support	Localisation	Section	Disponibilité	Etat_Exemplaire
049140	62-843 FLA	Papier	Bibliothèque Centrale	Génie Mécanique	Disponible	En bon état