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AGARD Conference Proceedings, N°600. Sustained Hypersonic Flight, volume 3 : Futur aerospace technology in the service of the Alliance; / AGARD Propulsion and Energetics Panel (PEP) (1997)
Titre de série : AGARD Conference Proceedings, N°600 Titre : Sustained Hypersonic Flight, volume 3 : Futur aerospace technology in the service of the Alliance; : Papers presented at the AGARD Symposium held at the Ecole Polytechnique, Palaiseau, France, 14-17 april 1997 Titre original : Le vol en croisière hypersonique, volume3 : Les Technologies aéronautiques et spatiales du futur au service de l'Alliance atlantique Type de document : texte imprimé Auteurs : AGARD Propulsion and Energetics Panel (PEP), Auteur Editeur : NATO - OTAN Année de publication : 1997 Collection : AGARD - Advisory Group for Aerospace Research and Development num. AGARD-CP-600 vol.3 Importance : pagination multiple Présentation : ill. noir&blanc, schémas Format : 29,5 x 21 cm Prix : Distribution of Unclassified AGARD Publications Langues : Anglais (eng) Français (fre) Catégories : Thésaurus AAE
Aéronautique (Ouvrages Généraux):Génie aéronautique:Mécanique et fonctionnement du vol aéronautiqueTags : hypersonic flight hypersonic vehicles scenarios,aerothermodynamics missile propulsion supersonic combustion ramjet engines ramjet engines design rochket propulsion combustion chambers hypersonic nozzles hypersonic characteristics hypersonic flow shock waves heat transfer military aircraft ramjet test vehicles thermal insulation film cooling ducted rocket engines military research test facilities flight tests airframes air intakes interactions combustion rockets fuels reviews Index. décimale : D.001.1 Mécanique et fonctionnement du vol aérospatial Résumé : Propulsion for hypersonic flight, external hypersonic aerodynamics and design challenges, military ramjet applications, test facilities for ramjets, configurational design and flight validation, engine/airframe integration, system challenges AGARD Conference Proceedings, N°600. Sustained Hypersonic Flight, volume 3 : Futur aerospace technology in the service of the Alliance; = Le vol en croisière hypersonique, volume3 : Les Technologies aéronautiques et spatiales du futur au service de l'Alliance atlantique : Papers presented at the AGARD Symposium held at the Ecole Polytechnique, Palaiseau, France, 14-17 april 1997 [texte imprimé] / AGARD Propulsion and Energetics Panel (PEP), Auteur . - [S.l.] : NATO - OTAN, 1997 . - pagination multiple : ill. noir&blanc, schémas ; 29,5 x 21 cm. - (AGARD - Advisory Group for Aerospace Research and Development; AGARD-CP-600 vol.3) .
Distribution of Unclassified AGARD Publications
Langues : Anglais (eng) Français (fre)
Catégories : Thésaurus AAE
Aéronautique (Ouvrages Généraux):Génie aéronautique:Mécanique et fonctionnement du vol aéronautiqueTags : hypersonic flight hypersonic vehicles scenarios,aerothermodynamics missile propulsion supersonic combustion ramjet engines ramjet engines design rochket propulsion combustion chambers hypersonic nozzles hypersonic characteristics hypersonic flow shock waves heat transfer military aircraft ramjet test vehicles thermal insulation film cooling ducted rocket engines military research test facilities flight tests airframes air intakes interactions combustion rockets fuels reviews Index. décimale : D.001.1 Mécanique et fonctionnement du vol aérospatial Résumé : Propulsion for hypersonic flight, external hypersonic aerodynamics and design challenges, military ramjet applications, test facilities for ramjets, configurational design and flight validation, engine/airframe integration, system challenges Réservation
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Code-barres Cote Support Localisation Section Disponibilité 201 D.001.1 AGA Ouvrages Centre de documentation Collection OTAN - NATO Disponible AGARD Report, 820. Active combustion control for propulsion systems / AGARD Propulsion and Energetics Panel (PEP) (1997) / 978-92-8361-060-1
Titre de série : AGARD Report, 820 Titre : Active combustion control for propulsion systems : A workshop held in Athens, Greec, may 6-9 1996 Titre original : Le contrôle actif de la combustion pour les systèmes de propulsion Type de document : texte imprimé Auteurs : AGARD Propulsion and Energetics Panel (PEP), Auteur Editeur : NATO - OTAN Année de publication : 1997 Collection : AGARD - Advisory Group for Aerospace Research and Development num. AGARD-R-820 Importance : pagination multiple Présentation : ill. noir&blanc, schémas Format : 29,5 x 21 cm ISBN/ISSN/EAN : 978-92-8361-060-1 Prix : Distribution of Unclassified AGARD Publications Langues : Anglais (eng) Catégories : Thésaurus AAE
Astronautique (Ouvrages Généraux):Génie astronautiqueTags : combustion control combustion chambers optimization rocket engines ramjet engines afterburners aircraft engines gas turbine engines stationary engines marine engines international cooperation combustion stability missile propulsion rocket propulsion incinerators Index. décimale : F.001.5 Système de propulsion Résumé : Active combustion control is one of the most promising approaches to further optimize the size/weight/power relationship in rockets, ramjets, afterburners, aero-engines, and marine propulsion. AGARD Report, 820. Active combustion control for propulsion systems = Le contrôle actif de la combustion pour les systèmes de propulsion : A workshop held in Athens, Greec, may 6-9 1996 [texte imprimé] / AGARD Propulsion and Energetics Panel (PEP), Auteur . - [S.l.] : NATO - OTAN, 1997 . - pagination multiple : ill. noir&blanc, schémas ; 29,5 x 21 cm. - (AGARD - Advisory Group for Aerospace Research and Development; AGARD-R-820) .
ISBN : 978-92-8361-060-1 : Distribution of Unclassified AGARD Publications
Langues : Anglais (eng)
Catégories : Thésaurus AAE
Astronautique (Ouvrages Généraux):Génie astronautiqueTags : combustion control combustion chambers optimization rocket engines ramjet engines afterburners aircraft engines gas turbine engines stationary engines marine engines international cooperation combustion stability missile propulsion rocket propulsion incinerators Index. décimale : F.001.5 Système de propulsion Résumé : Active combustion control is one of the most promising approaches to further optimize the size/weight/power relationship in rockets, ramjets, afterburners, aero-engines, and marine propulsion. Réservation
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Code-barres Cote Support Localisation Section Disponibilité 212 F.001.5 AGA Ouvrages Centre de documentation Collection OTAN - NATO Disponible AGARD Advisory Group, 201. Research and development of Ram/scramjets and turboramjets in Russia / AGARD Lecture Series (1993) / 978-92-8350-732-1
Titre de série : AGARD Advisory Group, 201 Titre : Research and development of Ram/scramjets and turboramjets in Russia Titre original : La recherche et le développement des Statoréacteurs, des statoréacteurs à combustion supersonique et des turboréacteurs en Russie Type de document : texte imprimé Auteurs : AGARD Lecture Series, Auteur Editeur : NATO - OTAN Année de publication : 1993 Collection : AGARD - Advisory Group for Aerospace Research and Development num. AGARD-LS-194 Importance : 232 p. Présentation : ill. noir & blanc, schémas Format : 30 x 21 cm ISBN/ISSN/EAN : 978-92-8350-732-1 Note générale : This publication was prepared at the request of the Structure and Materials Panel and under the sponsorship of the Consultant and Exchange Programme of AGARD and will be presented on 27-28 april 1995 in LIsbon, Portugal, 1-2 may 1995 in Eskisehir, Turkey, and 4-5 may 1995 in Ottobrun, Germany Langues : Anglais (eng) Catégories : Archives
8 AR-P.MARETags : ramjet engines solid rocket propellants liquid rocket propellants computational fluid dynamics Russia flight tests Index. décimale : 363.124 Risques dans les transports : Transports aérien et spatial Résumé : This lecture series will present and discuss the scientific problems of the development of ramjets/scramjets and turboramjets AGARD Advisory Group, 201. Research and development of Ram/scramjets and turboramjets in Russia = La recherche et le développement des Statoréacteurs, des statoréacteurs à combustion supersonique et des turboréacteurs en Russie [texte imprimé] / AGARD Lecture Series, Auteur . - [S.l.] : NATO - OTAN, 1993 . - 232 p. : ill. noir & blanc, schémas ; 30 x 21 cm. - (AGARD - Advisory Group for Aerospace Research and Development; AGARD-LS-194) .
ISBN : 978-92-8350-732-1
This publication was prepared at the request of the Structure and Materials Panel and under the sponsorship of the Consultant and Exchange Programme of AGARD and will be presented on 27-28 april 1995 in LIsbon, Portugal, 1-2 may 1995 in Eskisehir, Turkey, and 4-5 may 1995 in Ottobrun, Germany
Langues : Anglais (eng)
Catégories : Archives
8 AR-P.MARETags : ramjet engines solid rocket propellants liquid rocket propellants computational fluid dynamics Russia flight tests Index. décimale : 363.124 Risques dans les transports : Transports aérien et spatial Résumé : This lecture series will present and discuss the scientific problems of the development of ramjets/scramjets and turboramjets Exemplaires
Code-barres Cote Support Localisation Section Disponibilité 206 8-AR 363.124 AGA Ouvrages Bibliothèque d'archives de l'Académie AR - Donation MAREC Jean-Pierre Archives AAE-Donations
Exclu du prêtAGARD Advisory Group. Mathematical models of Gas Turbine Engines and their Components. / AGARD Lecture Series (1994)
Titre de série : AGARD Advisory Group Titre : Mathematical models of Gas Turbine Engines and their Components. Type de document : texte imprimé Auteurs : AGARD Lecture Series, Auteur Editeur : NATO - OTAN Année de publication : 1994 Collection : AGARD - Advisory Group for Aerospace Research and Development num. AGARD-LS-198 Importance : 192 p. Format : 21 x 30 cm. Langues : Anglais (eng) Catégories : Archives
8 AR-P.MARETags : Aircraft engines Gas turbine engines components Mathematical models aerodynamics Jet propulsion Numerical analysis Experimental data Thermal stresses Index. décimale : 363.124 Risques dans les transports : Transports aérien et spatial Résumé : This lecture series will present and discuss the scientific problems of modern mathematical simulation of gas turbine engines and their components. Some peculiarities of complex multicomponent and multidisciplinary models for whole flow passage of bypass gas turbine engine, core, multistage compressors and turbines, and other engine components will be studied. AGARD Advisory Group. Mathematical models of Gas Turbine Engines and their Components. [texte imprimé] / AGARD Lecture Series, Auteur . - [S.l.] : NATO - OTAN, 1994 . - 192 p. ; 21 x 30 cm.. - (AGARD - Advisory Group for Aerospace Research and Development; AGARD-LS-198) .
Langues : Anglais (eng)
Catégories : Archives
8 AR-P.MARETags : Aircraft engines Gas turbine engines components Mathematical models aerodynamics Jet propulsion Numerical analysis Experimental data Thermal stresses Index. décimale : 363.124 Risques dans les transports : Transports aérien et spatial Résumé : This lecture series will present and discuss the scientific problems of modern mathematical simulation of gas turbine engines and their components. Some peculiarities of complex multicomponent and multidisciplinary models for whole flow passage of bypass gas turbine engine, core, multistage compressors and turbines, and other engine components will be studied. Exemplaires
Code-barres Cote Support Localisation Section Disponibilité 3223 363.124 AGA Ouvrages Bibliothèque d'archives de l'Académie AR - Donation MAREC Jean-Pierre Archives AAE-Donations
Exclu du prêtAGARD Advisory Report. Integrated Vehicle Management Systems / AGARD Advisory Group (1996) / 978-92-8361-035-9
Titre de série : AGARD Advisory Report Titre : Integrated Vehicle Management Systems Titre original : Systèmes de gestion de vecteur intégré Type de document : texte imprimé Auteurs : AGARD Advisory Group, Auteur Editeur : NATO - OTAN Année de publication : 1996 Collection : AGARD - Advisory Group for Aerospace Research and Development num. AGARD-AR-343 Importance : 140 p. Format : 21 x 30 cm. ISBN/ISSN/EAN : 978-92-8361-035-9 Langues : Anglais (eng) Catégories : Archives
8 AR-P.MARETags : Technology Weapon systems Integrated systems Design Safety Navigation Propulsion Aircraft Helicopters Missiles UAV Index. décimale : 363.124 Risques dans les transports : Transports aérien et spatial Résumé : Major trends in technology, weapon system performance goals and affordability for aerospace systems are occuring simultaneously. For avionic systems this performance and affordability can be achieved by functional and physical integration. "Functionally" integrated systems to achieve higher performance has been greatly aided by advances in computer technology. The desire to minimize cost for these systems has been accomplished throught a "physical" integration concept based upon common modules tied through a "physical" concept, called integrated avionics, has been used on new aircraft such as the US Air Force F22 fighter and the Boeing 777 commercial transport. AGARD Advisory Report. Integrated Vehicle Management Systems = Systèmes de gestion de vecteur intégré [texte imprimé] / AGARD Advisory Group, Auteur . - [S.l.] : NATO - OTAN, 1996 . - 140 p. ; 21 x 30 cm.. - (AGARD - Advisory Group for Aerospace Research and Development; AGARD-AR-343) .
ISBN : 978-92-8361-035-9
Langues : Anglais (eng)
Catégories : Archives
8 AR-P.MARETags : Technology Weapon systems Integrated systems Design Safety Navigation Propulsion Aircraft Helicopters Missiles UAV Index. décimale : 363.124 Risques dans les transports : Transports aérien et spatial Résumé : Major trends in technology, weapon system performance goals and affordability for aerospace systems are occuring simultaneously. For avionic systems this performance and affordability can be achieved by functional and physical integration. "Functionally" integrated systems to achieve higher performance has been greatly aided by advances in computer technology. The desire to minimize cost for these systems has been accomplished throught a "physical" integration concept based upon common modules tied through a "physical" concept, called integrated avionics, has been used on new aircraft such as the US Air Force F22 fighter and the Boeing 777 commercial transport. Exemplaires
Code-barres Cote Support Localisation Section Disponibilité 145 8-AR 363.124 AGA Ouvrages Bibliothèque d'archives de l'Académie AR - Donation MAREC Jean-Pierre Archives AAE-Donations
Exclu du prêtAGARD Lecture Series, TCP 02/LS198. Mathematical models of gas turbine engines and their components / AGARD Propulsion and Energetics Panel (PEP) (1994) / 98-836-1008-3
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