Centre de documentation - Bibliothèque
Accueil
Catalogue bibliographique
A partir de cette page vous pouvez :
Retourner au premier écran avec les dernières notices... |
Résultat de la recherche
4 résultat(s) recherche sur le tag 'reliability'
Affiner la recherche
AGARD 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 Advisory Report. Technical evaluation report for the symposium on "active" control systems - Review, evaluation and projections" / AGARD Advisory Group (1985)
Titre de série : AGARD Advisory Report Titre : Technical evaluation report for the symposium on "active" control systems - Review, evaluation and projections" Type de document : texte imprimé Auteurs : AGARD Advisory Group, Auteur Editeur : NATO - OTAN Année de publication : 1985 Collection : AGARD - Advisory Group for Aerospace Research and Development num. AGARD-AR-220 Importance : 18 p. Format : 21 x 30 cm. Langues : Anglais (eng) Catégories : Archives
8 AR-P.MARETags : active control Flight control Flight characteristic Systems engineering Control theory Reliability Index. décimale : 363.124 Risques dans les transports : Transports aérien et spatial Résumé : The Symposium was held in toronto, Canada, during 15 - 18 October, 1984. It was attended by 148 people. 27 papers were ^presented on various topics related to active control technology. The meeting was highlighted by a number of reports on actual flight test experience with active control systems. The contents of the papers taken as a group provide an extremely useful summary of current knowledge in the field and indicate the direction that future research should take. AGARD Advisory Report. Technical evaluation report for the symposium on "active" control systems - Review, evaluation and projections" [texte imprimé] / AGARD Advisory Group, Auteur . - [S.l.] : NATO - OTAN, 1985 . - 18 p. ; 21 x 30 cm.. - (AGARD - Advisory Group for Aerospace Research and Development; AGARD-AR-220) .
Langues : Anglais (eng)
Catégories : Archives
8 AR-P.MARETags : active control Flight control Flight characteristic Systems engineering Control theory Reliability Index. décimale : 363.124 Risques dans les transports : Transports aérien et spatial Résumé : The Symposium was held in toronto, Canada, during 15 - 18 October, 1984. It was attended by 148 people. 27 papers were ^presented on various topics related to active control technology. The meeting was highlighted by a number of reports on actual flight test experience with active control systems. The contents of the papers taken as a group provide an extremely useful summary of current knowledge in the field and indicate the direction that future research should take. Exemplaires
Code-barres Cote Support Localisation Section Disponibilité 3137 8-AR 363.124 AGA Ouvrages Bibliothèque d'archives de l'Académie AR - Donation MAREC Jean-Pierre Archives AAE-Donations
Exclu du prêtRTO 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
Réserver ce document
Exemplaires
Code-barres Cote Support Localisation Section Disponibilité 231 D.004 RTO Ouvrages Centre de documentation Collection OTAN - NATO Disponible RTO Technical Report, N°13. Life cycle cost of all-electric combat vehicles / RTO Studies, Analysis and simulation panel (SAS) (1999)
Titre de série : RTO Technical Report, N°13 Titre : Life cycle cost of all-electric combat vehicles : This long-term scientific study was managed by the Studies, Analysis and Simulation Panel (SAS) Titre original : Coûts globaux de possession des véhicules de combat tout-électriques Type de document : texte imprimé Auteurs : RTO Studies, Analysis and simulation panel (SAS), Auteur Editeur : NATO - OTAN Année de publication : 1999 Collection : RTO Research and Technology Organisation num. RTO-TR-13 Importance : pagination multiple Présentation : ill. noir&blanc, schémas Format : 29,5 x 21 cm Prix : Distribution of Unclassified RTO Publications Langues : Anglais (eng) Catégories : Thésaurus AAE
Armée (Ouvrages Généraux)Tags : electric vehicles combat vehicles service life life cycle costs defense economics performance electric power mobility survivability lethability reliability prototypes statistical data cost analysis mathematical models NATO signature reduction Index. décimale : C.002 Génie Militaire (Construction) Résumé : Reports a long term scientific study to evaluate the Life-Cycle-Cost (LCC) of a possible future All-Electric Combat Vehicule (AECV), to be fielded in 2015. RTO Technical Report, N°13. Life cycle cost of all-electric combat vehicles = Coûts globaux de possession des véhicules de combat tout-électriques : This long-term scientific study was managed by the Studies, Analysis and Simulation Panel (SAS) [texte imprimé] / RTO Studies, Analysis and simulation panel (SAS), Auteur . - [S.l.] : NATO - OTAN, 1999 . - pagination multiple : ill. noir&blanc, schémas ; 29,5 x 21 cm. - (RTO Research and Technology Organisation; RTO-TR-13) .
Distribution of Unclassified RTO Publications
Langues : Anglais (eng)
Catégories : Thésaurus AAE
Armée (Ouvrages Généraux)Tags : electric vehicles combat vehicles service life life cycle costs defense economics performance electric power mobility survivability lethability reliability prototypes statistical data cost analysis mathematical models NATO signature reduction Index. décimale : C.002 Génie Militaire (Construction) Résumé : Reports a long term scientific study to evaluate the Life-Cycle-Cost (LCC) of a possible future All-Electric Combat Vehicule (AECV), to be fielded in 2015. Réservation
Réserver ce document
Exemplaires
Code-barres Cote Support Localisation Section Disponibilité 240 C.002 RTO Ouvrages Centre de documentation Collection OTAN - NATO Disponible
Recherches dans d'autres bibliothèques et centres de ressources : |
||
AAE
pmb