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Gas turbine propulsion systems / MacIsaac, Bernie

Public ISBD Titre : Gas turbine propulsion systems Type de document : texte imprimé Auteurs : MacIsaac, Bernie, Auteur ; Langton, Roy, Auteur Editeur : New York : Wiley Année de publication : 2011 Importance : 328 p. Présentation : ill. Format : 25 cm ISBN/ISSN/EAN : 978-0-470-06563-1 Note générale : Notes bibliogr. - Index Langues : Anglais (eng) Mots-clés : Aircraft  gas-turbines Airplanes  --  Turbojet  engines Jet  boat  engines Vehicles,  Military Véhicules  militaires Avions  --  Turboréacteurs Index. décimale : 621.438 Turbines de combustion.Turbines à gaz.Turbines à huile Résumé : Gas Turbine Propulsion Systems in Aerospace & Defense' pulls together all of the systems and subsystems associated with gas turbine engines in aircraft and marine warship applications. The subject of engine (fuel) control has undergone major changes in the past 20 years due to the advent of the digital electronic control technology and therefore existing books on the subject are typically out of date with current methods. 'Gas Turbine Propulsion Systems in Aerospace & Defense' discusses the latest technologies in this area; including marine propulsion which is an emerging application area for the technology that involves some interesting modifications to aviation technologies. This book also fits well into the systems engineering focus of the Aerospace Series. Includes chapters on aircraft engine systems functional overview, marine propulsion systems, fuel control and power management systems, engine lubrication and scavenging systems, nacelle and ancillary systems, engine certification, unique engine systems and future developments in gas turbine propulsion systems Includes case studies of specific engines Includes applications within marine defence Accompanied by a book companion website featuring full colour images "-- "This book also fits well into the systems engineering focus of the Aerospace Series" Note de contenu : In summary : 1. Basic gas turbine operation. 2. Gas generator fuel control systems. 3. Thrust engine control and augmentation systems. 4. Shaft power propulsion control systems. 5. Engine inlet, exhaust, and nacelle systems. 6. Lubrication systems. 7. Power extraction and starting systems. 8. Marine propulsion systems. 9. Prognostics and health monitoring systems. 10. New and future gas turbine propulsion system technologies. ... Gas turbine propulsion systems [texte imprimé] / MacIsaac, Bernie, Auteur ; Langton, Roy, Auteur . - New York : Wiley, 2011 . - 328 p. : ill. ; 25 cm. ISBN : 978-0-470-06563-1 Notes bibliogr. - Index Langues : Anglais (eng) Mots-clés : Aircraft  gas-turbines Airplanes  --  Turbojet  engines Jet  boat  engines Vehicles,  Military Véhicules  militaires Avions  --  Turboréacteurs Index. décimale : 621.438 Turbines de combustion.Turbines à gaz.Turbines à huile Résumé : Gas Turbine Propulsion Systems in Aerospace & Defense' pulls together all of the systems and subsystems associated with gas turbine engines in aircraft and marine warship applications. The subject of engine (fuel) control has undergone major changes in the past 20 years due to the advent of the digital electronic control technology and therefore existing books on the subject are typically out of date with current methods. 'Gas Turbine Propulsion Systems in Aerospace & Defense' discusses the latest technologies in this area; including marine propulsion which is an emerging application area for the technology that involves some interesting modifications to aviation technologies. This book also fits well into the systems engineering focus of the Aerospace Series. Includes chapters on aircraft engine systems functional overview, marine propulsion systems, fuel control and power management systems, engine lubrication and scavenging systems, nacelle and ancillary systems, engine certification, unique engine systems and future developments in gas turbine propulsion systems Includes case studies of specific engines Includes applications within marine defence Accompanied by a book companion website featuring full colour images "-- "This book also fits well into the systems engineering focus of the Aerospace Series" Note de contenu : In summary : 1. Basic gas turbine operation. 2. Gas generator fuel control systems. 3. Thrust engine control and augmentation systems. 4. Shaft power propulsion control systems. 5. Engine inlet, exhaust, and nacelle systems. 6. Lubrication systems. 7. Power extraction and starting systems. 8. Marine propulsion systems. 9. Prognostics and health monitoring systems. 10. New and future gas turbine propulsion system technologies. ...

Exemplaires

Code-barres	Cote	Support	Localisation	Section	Disponibilité	Etat_Exemplaire
053727	621.438 MAC	Papier	Bibliothèque Centrale	Génie Mécanique	Disponible	Consultation sur place

Stability and control of aircraft systems / Langton, Roy

Public ISBD Titre : Stability and control of aircraft systems : introduction to classical feedback control Type de document : texte imprimé Auteurs : Langton, Roy, Auteur Editeur : New York : Wiley Année de publication : 2006 Collection : Aerospace series Importance : 238 p. Présentation : ill. Format : 24 cm ISBN/ISSN/EAN : 978-0-470-01891-0 Note générale : Index Langues : Français (fre) Mots-clés : Stability  of  airplanes Airplanes  --  Control Avions  --  Stabilité Avions  --  Systèmes  de  commande Index. décimale : 629.7 Ingénierie du transport aérien et spatial.Aéronautique et aéronefs.Fusées et missiles.Astronautique et engins spatiaux Résumé : In the current climate of increasing complexity and functional integration in all areas of engineering and technology, stability and control are becoming essential ingredients of engineering knowledge. Many of today's products contain multiple engineering technologies, and what were once simple mechanical, hydraulic or pneumatic products now contain integrated electronics and sensors. Control theory reduces these widely varied technical components into their important dynamic characteristics, expressed as transfer functions, from which the subtleties of dynamic behaviours can be analyzed and understood. Stability and Control of Aircraft Systems is an easy-to-read and understand text that describes control theory using minimal mathematics. It focuses on simple rules, tools and methods for the analysis and testing of feedback control systems using real systems engineering design and development examples.* Clarifies the design and development of feedback control systems * Communicates the theory in an accessible manner that does not require the reader to have a strong mathematical background * Illustrated throughout with figures and tables Stability and Control of Aircraft Systems provides both the seasoned engineer and the graduate with the know-how necessary to minimize problems with fielded systems in the area of operational performance Stability and control of aircraft systems : introduction to classical feedback control [texte imprimé] / Langton, Roy, Auteur . - Wiley, 2006 . - 238 p. : ill. ; 24 cm. - (Aerospace series) . ISBN : 978-0-470-01891-0 Index Langues : Français (fre) Mots-clés : Stability  of  airplanes Airplanes  --  Control Avions  --  Stabilité Avions  --  Systèmes  de  commande Index. décimale : 629.7 Ingénierie du transport aérien et spatial.Aéronautique et aéronefs.Fusées et missiles.Astronautique et engins spatiaux Résumé : In the current climate of increasing complexity and functional integration in all areas of engineering and technology, stability and control are becoming essential ingredients of engineering knowledge. Many of today's products contain multiple engineering technologies, and what were once simple mechanical, hydraulic or pneumatic products now contain integrated electronics and sensors. Control theory reduces these widely varied technical components into their important dynamic characteristics, expressed as transfer functions, from which the subtleties of dynamic behaviours can be analyzed and understood. Stability and Control of Aircraft Systems is an easy-to-read and understand text that describes control theory using minimal mathematics. It focuses on simple rules, tools and methods for the analysis and testing of feedback control systems using real systems engineering design and development examples.* Clarifies the design and development of feedback control systems * Communicates the theory in an accessible manner that does not require the reader to have a strong mathematical background * Illustrated throughout with figures and tables Stability and Control of Aircraft Systems provides both the seasoned engineer and the graduate with the know-how necessary to minimize problems with fielded systems in the area of operational performance

Exemplaires

Code-barres	Cote	Support	Localisation	Section	Disponibilité	Etat_Exemplaire
053757	629.7 LAN	Papier	Bibliothèque Centrale	Ingénierie	Disponible	Consultation sur place