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AGARD Advisory Report. Hypersonic Experimental and Computational Capability, Improvement and Validation / AGARD Advisory Group (1998) / 978-92-8361-078-6
Titre de série : AGARD Advisory Report Titre : Hypersonic Experimental and Computational Capability, Improvement and Validation 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-319 Vol. II Importance : 172 p. Format : 21 x 30 cm. ISBN/ISSN/EAN : 978-92-8361-078-6 Langues : Anglais (eng) Catégories : Archives
8 AR-P.MARETags : Experimentation Research projects Hypersonic flow Test facilities Rarefied gas dynamics shock waves Transition Flow Lauch vehicles Index. décimale : 363.124 Risques dans les transports : Transports aérien et spatial Résumé : The results of the phase II effort conducted under AGARD Working Group 18 on Hypersonic Experimental and Computational Capabiblity, Improvement and Validation are presented in this report. The first volume, published in May 1996, mainly focused on the design methodology, plans and some initial results of experiments that had been conducted to serve as validation benchmarks. The current volume presents the detailed experimental and computational data base developed during this effort. AGARD Advisory Report. Hypersonic Experimental and Computational Capability, Improvement and Validation [texte imprimé] / AGARD Advisory Group, Auteur . - [S.l.] : NATO - OTAN, 1998 . - 172 p. ; 21 x 30 cm.. - (AGARD - Advisory Group for Aerospace Research and Development; AGARD-AR-319 Vol. II) .
ISBN : 978-92-8361-078-6
Langues : Anglais (eng)
Catégories : Archives
8 AR-P.MARETags : Experimentation Research projects Hypersonic flow Test facilities Rarefied gas dynamics shock waves Transition Flow Lauch vehicles Index. décimale : 363.124 Risques dans les transports : Transports aérien et spatial Résumé : The results of the phase II effort conducted under AGARD Working Group 18 on Hypersonic Experimental and Computational Capabiblity, Improvement and Validation are presented in this report. The first volume, published in May 1996, mainly focused on the design methodology, plans and some initial results of experiments that had been conducted to serve as validation benchmarks. The current volume presents the detailed experimental and computational data base developed during this effort. Exemplaires
Code-barres Cote Support Localisation Section Disponibilité 2906 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. A Selection of Test Cases for the Validation of Large-Eddy Simulations of Turbulent Flows. / AGARD Advisory Group (1998) / 978-92-8361-072-4
Titre de série : AGARD Advisory Report Titre : A Selection of Test Cases for the Validation of Large-Eddy Simulations of Turbulent Flows. 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-345 Importance : 212 p. Présentation : schémas Format : 21 x 30 cm. ISBN/ISSN/EAN : 978-92-8361-072-4 Langues : Anglais (eng) Catégories : Archives
8 AR-P.MARETags : Eddies Turbulent flow Simulation Turbulence Shear flow Boundary layer Pipes Channel flow Jet flow Jets Two dimensional flow Pressure gradients Incomprehensove flow Shock waves Computerized simulation Tests Experimentation Proving Index. décimale : 363.124 Risques dans les transports : Transports aérien et spatial Résumé : The result of the AGARD FDP Working Group 21 on a Selection of Test Cases for the Validation of Large-Eddy Simulations of Turbulent Flows are presented in this report. The data contained in the report consist of building-block experiments documented in as much detail as posssible. They are useful for the validation of Reynold Averaged modeling and for the preliminary evaluation of experiments or turbulence theories. They include both laboratory experiments and direct numerical simulations. Note de contenu : CD-ROM
Lettre expliquant l’intégration d'un CD-ROM dans l'ouvrage.AGARD Advisory Report. A Selection of Test Cases for the Validation of Large-Eddy Simulations of Turbulent Flows. [texte imprimé] / AGARD Advisory Group, Auteur . - [S.l.] : NATO - OTAN, 1998 . - 212 p. : schémas ; 21 x 30 cm.. - (AGARD - Advisory Group for Aerospace Research and Development; AGARD-AR-345) .
ISBN : 978-92-8361-072-4
Langues : Anglais (eng)
Catégories : Archives
8 AR-P.MARETags : Eddies Turbulent flow Simulation Turbulence Shear flow Boundary layer Pipes Channel flow Jet flow Jets Two dimensional flow Pressure gradients Incomprehensove flow Shock waves Computerized simulation Tests Experimentation Proving Index. décimale : 363.124 Risques dans les transports : Transports aérien et spatial Résumé : The result of the AGARD FDP Working Group 21 on a Selection of Test Cases for the Validation of Large-Eddy Simulations of Turbulent Flows are presented in this report. The data contained in the report consist of building-block experiments documented in as much detail as posssible. They are useful for the validation of Reynold Averaged modeling and for the preliminary evaluation of experiments or turbulence theories. They include both laboratory experiments and direct numerical simulations. Note de contenu : CD-ROM
Lettre expliquant l’intégration d'un CD-ROM dans l'ouvrage.Exemplaires
Code-barres Cote Support Localisation Section Disponibilité 2912 8-AR 363.124 AGA Ouvrages Bibliothèque d'archives de l'Académie AR - Donation MAREC Jean-Pierre Archives AAE-Donations
Exclu du prêtAGARD 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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Exemplaires
Code-barres Cote Support Localisation Section Disponibilité 201 D.001.1 AGA Ouvrages Centre de documentation Collection OTAN - NATO Disponible AGARD Advisory Group. Human Consequences of Agile Aircraft / AGARD Éducational Notes (2000) / 978-92-8371-030-1
Titre de série : AGARD Advisory Group Titre : Human Consequences of Agile Aircraft Type de document : texte imprimé Auteurs : AGARD Éducational Notes, Auteur Editeur : NATO - OTAN Année de publication : 2000 Collection : AGARD - Advisory Group for Aerospace Research and Development num. RTO-EN-8 AC/323 (AVT) TP23 Importance : 400 p. Format : 21 x 30 cm. ISBN/ISSN/EAN : 978-92-8371-030-1 Langues : Anglais (eng) Catégories : Archives
8 AR-P.MARETags : Enthalpy Heat measurement Temperature measuring instruments Plasmas Catalysis Test facilities Shock tubes Diagnosis Hypersonic flow Heat transfer Index. décimale : 363.124 Risques dans les transports : Transports aérien et spatial Résumé : The following topics were covered:
-Review of various high enthalpy and plasma flow facilities,
-Intrusive and non intrusive measurement techniques for the characterization of the flows generated in these facilities,
-utilization of the plasma facilities forthe evaluation of material catalytic properties.AGARD Advisory Group. Human Consequences of Agile Aircraft [texte imprimé] / AGARD Éducational Notes, Auteur . - [S.l.] : NATO - OTAN, 2000 . - 400 p. ; 21 x 30 cm.. - (AGARD - Advisory Group for Aerospace Research and Development; RTO-EN-8 AC/323 (AVT) TP23) .
ISBN : 978-92-8371-030-1
Langues : Anglais (eng)
Catégories : Archives
8 AR-P.MARETags : Enthalpy Heat measurement Temperature measuring instruments Plasmas Catalysis Test facilities Shock tubes Diagnosis Hypersonic flow Heat transfer Index. décimale : 363.124 Risques dans les transports : Transports aérien et spatial Résumé : The following topics were covered:
-Review of various high enthalpy and plasma flow facilities,
-Intrusive and non intrusive measurement techniques for the characterization of the flows generated in these facilities,
-utilization of the plasma facilities forthe evaluation of material catalytic properties.Exemplaires
Code-barres Cote Support Localisation Section Disponibilité 3288 8-AR 363.124 AGA Ouvrages Bibliothèque d'archives de l'Académie AR - Donation MAREC Jean-Pierre Archives AAE-Donations
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