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AGARD 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. CFD Validation for propulsion System Components / AGARD Advisory Group (1998) / 978-92-8361-075-5
Titre de série : AGARD Advisory Report Titre : CFD Validation for propulsion System Components Type de document : texte imprimé Auteurs : AGARD Advisory Group, Auteur Editeur : NATO - OTAN Année de publication : 1998 Collection : AGARD - Advisory Group for Aerospace Research and Development num. AGARD-AR-355 Importance : 96 p. Format : 21 x 30 cm. ISBN/ISSN/EAN : 978-92-8361-075-5 Langues : Anglais (eng) Catégories : Archives
8 AR-P.MARETags : Aircraft engines Gas turbine engines Design Computerized simulation Performance Reliability Gas flow Computational fluid dynamics Coding Navier-Stokkes equations Validity Turbomachinery Computation Turbulence Predictions Index. décimale : 363.124 Risques dans les transports : Transports aérien et spatial Résumé : Computer codes which solve the Reynolds-averaged Navier -Stokes equations are now used by manufacturers to design turbomachines, but there is no consensus about which grids and wwhich turbulence models are good enough to provide a reliable basis for design decisions. The AGARD Propulsion and Energetics Panel set up Working Group 26 to help to clarify these issues, by analysing predictions (using as wide a range of codes as possible) of two representative but difficult single blade row test cases: NASA Rotor 37 and an annular turbine cascade tested by DLR. This report presents the group's results and conclusions. AGARD Advisory Report. CFD Validation for propulsion System Components [texte imprimé] / AGARD Advisory Group, Auteur . - [S.l.] : NATO - OTAN, 1998 . - 96 p. ; 21 x 30 cm.. - (AGARD - Advisory Group for Aerospace Research and Development; AGARD-AR-355) .
ISBN : 978-92-8361-075-5
Langues : Anglais (eng)
Catégories : Archives
8 AR-P.MARETags : Aircraft engines Gas turbine engines Design Computerized simulation Performance Reliability Gas flow Computational fluid dynamics Coding Navier-Stokkes equations Validity Turbomachinery Computation Turbulence Predictions Index. décimale : 363.124 Risques dans les transports : Transports aérien et spatial Résumé : Computer codes which solve the Reynolds-averaged Navier -Stokes equations are now used by manufacturers to design turbomachines, but there is no consensus about which grids and wwhich turbulence models are good enough to provide a reliable basis for design decisions. The AGARD Propulsion and Energetics Panel set up Working Group 26 to help to clarify these issues, by analysing predictions (using as wide a range of codes as possible) of two representative but difficult single blade row test cases: NASA Rotor 37 and an annular turbine cascade tested by DLR. This report presents the group's results and conclusions. Exemplaires
Code-barres Cote Support Localisation Section Disponibilité 2901 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
Titre de série : AGARD Lecture Series, TCP 02/LS198 Titre : Mathematical models of gas turbine engines and their components : This publication was prepared at the request of the Propulsion and Energetics Panel of AGARD and under the sponsorship of the technology cooperatoin programme (NACC/Pfp) and will be presented on 7-8 december 1994 in Cleveland, USA, 12-13 december 1994 in Wessling, Germany, fand 15-16 december 1994 in Paris, France Titre original : Les modèles mathématiques des turbomoteurs et de leurs organes Type de document : texte imprimé Auteurs : AGARD Propulsion and Energetics Panel (PEP), Auteur Editeur : NATO - OTAN Année de publication : 1994 Collection : AGARD - Advisory Group for Aerospace Research and Development num. AGARD-LS-198 Importance : pagination multiple Présentation : ill. noir&blanc, schémas, Format : 29,5 x 21 cm ISBN/ISSN/EAN : 98-836-1008-3 Prix : Distribution of Unclassified AGARD Publications Langues : Anglais (eng) Catégories : Thésaurus AAE
Aéronautique (Ouvrages Généraux)Tags : aircraft engines gas turbine engines components mathematical models aerodynamics jet propulsion numerical analysis experimental data thermal stresses Index. décimale : D.001 Génie Aéronautique Résumé : This lecture series will present and discuss the scientific problems of modern mathematical simulation of gas turbine engines and their components AGARD Lecture Series, TCP 02/LS198. Mathematical models of gas turbine engines and their components = Les modèles mathématiques des turbomoteurs et de leurs organes : This publication was prepared at the request of the Propulsion and Energetics Panel of AGARD and under the sponsorship of the technology cooperatoin programme (NACC/Pfp) and will be presented on 7-8 december 1994 in Cleveland, USA, 12-13 december 1994 in Wessling, Germany, fand 15-16 december 1994 in Paris, France [texte imprimé] / AGARD Propulsion and Energetics Panel (PEP), Auteur . - [S.l.] : NATO - OTAN, 1994 . - pagination multiple : ill. noir&blanc, schémas, ; 29,5 x 21 cm. - (AGARD - Advisory Group for Aerospace Research and Development; AGARD-LS-198) .
ISSN : 98-836-1008-3 : Distribution of Unclassified AGARD Publications
Langues : Anglais (eng)
Catégories : Thésaurus AAE
Aéronautique (Ouvrages Généraux)Tags : aircraft engines gas turbine engines components mathematical models aerodynamics jet propulsion numerical analysis experimental data thermal stresses Index. décimale : D.001 Génie Aéronautique Résumé : This lecture series will present and discuss the scientific problems of modern mathematical simulation of gas turbine engines and their components Réservation
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Code-barres Cote Support Localisation Section Disponibilité 208 D.001 AGA Ouvrages Centre de documentation Collection OTAN - NATO Disponible RTO Meeting proceedings, 17. Qualification of life extension schemes for engine components / RTO Applied Vehicule Technology (AVT) (1999) / 978-92-8371-012-7
Titre de série : RTO Meeting proceedings, 17 Titre : Qualification of life extension schemes for engine components : Papers presented at the Work of the RTO Applied Vehicule Technology Panel (AVT) - organised by the former AGARD Structures and Materials Panel- held in Corfu, Greece, 5-6 october 1998 Titre original : Homologation des programmes de prolongation du cycle de vie des organes moteur Type de document : texte imprimé Auteurs : RTO Applied Vehicule Technology (AVT), Auteur Editeur : NATO - OTAN Année de publication : 1999 Collection : RTO Research and Technology Organisation num. RTO-MP-17 AC/323(AVT)TP/17 Importance : pagination multiple Présentation : ill. noir&blanc, schémas, photos Format : 29.5 x 21 cm ISBN/ISSN/EAN : 978-92-8371-012-7 Prix : Distribution of Unclassified RTO Publications Langues : Anglais (eng) Catégories : Thésaurus AAE
Aéronautique (Ouvrages Généraux):Génie aéronautique:Mécanique et fonctionnement du vol aéronautiqueTags : aircraft engines service life life cycle costs defense economics damage control durability performance reliability materials replacement protective coatings reconditioning maintenance design safety engineering tolerances (mechanics) fatigue (materials) cost effectiveness benefit cost analysis turbine components Index. décimale : D.004 Partie constituante d'aéronef ou d'avion Résumé : The replacementcost of service-damaged components contributes significantly to the life cycle costs of an aero-engine. Damaged engine components also impact on the realibility and safety of aircraft. RTO Meeting proceedings, 17. Qualification of life extension schemes for engine components = Homologation des programmes de prolongation du cycle de vie des organes moteur : Papers presented at the Work of the RTO Applied Vehicule Technology Panel (AVT) - organised by the former AGARD Structures and Materials Panel- held in Corfu, Greece, 5-6 october 1998 [texte imprimé] / RTO Applied Vehicule Technology (AVT), Auteur . - [S.l.] : NATO - OTAN, 1999 . - pagination multiple : ill. noir&blanc, schémas, photos ; 29.5 x 21 cm. - (RTO Research and Technology Organisation; RTO-MP-17 AC/323(AVT)TP/17) .
ISBN : 978-92-8371-012-7 : Distribution of Unclassified RTO Publications
Langues : Anglais (eng)
Catégories : Thésaurus AAE
Aéronautique (Ouvrages Généraux):Génie aéronautique:Mécanique et fonctionnement du vol aéronautiqueTags : aircraft engines service life life cycle costs defense economics damage control durability performance reliability materials replacement protective coatings reconditioning maintenance design safety engineering tolerances (mechanics) fatigue (materials) cost effectiveness benefit cost analysis turbine components Index. décimale : D.004 Partie constituante d'aéronef ou d'avion Résumé : The replacementcost of service-damaged components contributes significantly to the life cycle costs of an aero-engine. Damaged engine components also impact on the realibility and safety of aircraft. Réservation
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Exemplaires
Code-barres Cote Support Localisation Section Disponibilité 231 D.004 RTO Ouvrages Centre de documentation Collection OTAN - NATO Disponible AGARD Advisory Group, 217. Planar optical measurement methods for gas turbine components / AGARD Lecture Series (1999) / 978-92-8371-019-6
Titre de série : AGARD Advisory Group, 217 Titre : Planar optical measurement methods for gas turbine components Titre original : Méthode de mesure optiques planaires pour organes de turbomoteurs Type de document : texte imprimé Auteurs : AGARD Lecture Series, Auteur Editeur : NATO - OTAN Année de publication : 1999 Collection : RTO Research and Technology Organisation num. RTO-EN-6 AC/323(AVT)TP/20 Importance : 146 p. Présentation : ill. noir & blanc, schémas, photos ISBN/ISSN/EAN : 978-92-8371-019-6 Note générale : The Applied Vehicule Technologie panel (AVT) presented on 16-17 september 1999 in Cranfield, UK and 21-22 september 1999 in Cleveland, USA Langues : Anglais (eng) Catégories : Archives
8 AR-P.MARETags : optical measurement aircraft engines gas turbine engines laser doppler velocimetry flow visualization measuring instruments lasers planar devices velocity measurement PIV (particle image velocimetry) paints pressure sensors temperature measuring instruments laser induced fluorescence fuels drops (liquids) soot tests test facilities cost engineering Index. décimale : 363.124 Risques dans les transports : Transports aérien et spatial Résumé : This lecture series covers the recent advances of planar optical measurement techniques with respect to their applicability to gas turbine components tests. AGARD Advisory Group, 217. Planar optical measurement methods for gas turbine components = Méthode de mesure optiques planaires pour organes de turbomoteurs [texte imprimé] / AGARD Lecture Series, Auteur . - [S.l.] : NATO - OTAN, 1999 . - 146 p. : ill. noir & blanc, schémas, photos. - (RTO Research and Technology Organisation; RTO-EN-6 AC/323(AVT)TP/20) .
ISBN : 978-92-8371-019-6
The Applied Vehicule Technologie panel (AVT) presented on 16-17 september 1999 in Cranfield, UK and 21-22 september 1999 in Cleveland, USA
Langues : Anglais (eng)
Catégories : Archives
8 AR-P.MARETags : optical measurement aircraft engines gas turbine engines laser doppler velocimetry flow visualization measuring instruments lasers planar devices velocity measurement PIV (particle image velocimetry) paints pressure sensors temperature measuring instruments laser induced fluorescence fuels drops (liquids) soot tests test facilities cost engineering Index. décimale : 363.124 Risques dans les transports : Transports aérien et spatial Résumé : This lecture series covers the recent advances of planar optical measurement techniques with respect to their applicability to gas turbine components tests. Exemplaires
Code-barres Cote Support Localisation Section Disponibilité 225 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. Engine-airframe integration for rotorcraft / AGARD Lecture Series (1986)
PermalinkAGARD Advisory Group. Future Aerospace Technology int he Service of the Alliance: Affordable Combat aircraft / AGARD Conférence Proceeding (1997)
PermalinkAGARD Advisory Group. Integrated Multidisciplinary Design of High Pressure Multistage Compressor Systems / AGARD Lecture Series (1998) / 978-92-8371-000-4
PermalinkAGARD Advisory Group. Turbomachinery design using CFD / AGARD Lecture Series (1994) / 978-92-8350-749-9
PermalinkAGARD Advisory Report. Microprocessor Applications in airborne flight test instrumentation / AGARD Flight (1987)
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