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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. A selection of Experimental Test Cases for the Validation of CFD Codes / AGARD Advisory Group (1994) / 978-92-8361-002-1
Titre de série : AGARD Advisory Report Titre : A selection of Experimental Test Cases for the Validation of CFD Codes Type de document : texte imprimé Auteurs : AGARD Advisory Group, Auteur Editeur : NATO - OTAN Année de publication : 1994 Collection : AGARD - Advisory Group for Aerospace Research and Development num. AGARD-AR-303 Volume 1 Importance : 156 p. Format : 21 x 30 cm. ISBN/ISSN/EAN : 978-92-8361-002-1 Langues : Anglais (eng) Catégories : Archives
8 AR-P.MARETags : Computational fluid dynamics Aerodynamic configurations Aircraft Missiles Wind tunnel test Data bases Validity Index. décimale : 363.124 Risques dans les transports : Transports aérien et spatial Résumé : This report presents the results of a study by Working Group 14 of the AGARD Fluid Dynamics Panel. This group was formed to establish an accessible, detailed experimental data base for the validation of Fluid Dynamics (CFD) codes. AGARD Advisory Report. A selection of Experimental Test Cases for the Validation of CFD Codes [texte imprimé] / AGARD Advisory Group, Auteur . - [S.l.] : NATO - OTAN, 1994 . - 156 p. ; 21 x 30 cm.. - (AGARD - Advisory Group for Aerospace Research and Development; AGARD-AR-303 Volume 1) .
ISBN : 978-92-8361-002-1
Langues : Anglais (eng)
Catégories : Archives
8 AR-P.MARETags : Computational fluid dynamics Aerodynamic configurations Aircraft Missiles Wind tunnel test Data bases Validity Index. décimale : 363.124 Risques dans les transports : Transports aérien et spatial Résumé : This report presents the results of a study by Working Group 14 of the AGARD Fluid Dynamics Panel. This group was formed to establish an accessible, detailed experimental data base for the validation of Fluid Dynamics (CFD) codes. Exemplaires
Code-barres Cote Support Localisation Section Disponibilité 3132 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 Experimental Test Cases for the Validation of CFD Codes / AGARD Advisory Group (1994)
Titre de série : AGARD Advisory Report Titre : A selection of Experimental Test Cases for the Validation of CFD Codes Type de document : texte imprimé Auteurs : AGARD Advisory Group, Auteur Editeur : NATO - OTAN Année de publication : 1994 Collection : AGARD - Advisory Group for Aerospace Research and Development num. AGARD-AR-303 Volume 2 Importance : 596 p. Format : 21 x 30 cm. Langues : Anglais (eng) Catégories : Archives
8 AR-P.MARETags : Aircraft missiles Validity Data bases Aerodynamic configurations Computational fluid dynamics Wind tunnel test Index. décimale : 363.124 Risques dans les transports : Transports aérien et spatial Résumé : This report presents the results of a study by Working Group 14 of the AGARD Fluid Dynamics Panel. This group was formed to establish an accessible, detailed experimental data base for the validation of Fluid Dynamics (CFD) codes.
The thirty nine test cases are documented cover the subsonic, transonic; and supersonic flow regimes and five classes of geometries. Included in the five classes of geometries are: Two Dimensional Airfoils; Three Dimensional Wings, designed for predominantly attached flow conditions; Slender Bodies, typical of missile type configurations; Delta Wings, characterized by a conical type of vortex flow; and Complex Configurations, either in a geometrical sense or because of complicated flow onteractions.AGARD Advisory Report. A selection of Experimental Test Cases for the Validation of CFD Codes [texte imprimé] / AGARD Advisory Group, Auteur . - [S.l.] : NATO - OTAN, 1994 . - 596 p. ; 21 x 30 cm.. - (AGARD - Advisory Group for Aerospace Research and Development; AGARD-AR-303 Volume 2) .
Langues : Anglais (eng)
Catégories : Archives
8 AR-P.MARETags : Aircraft missiles Validity Data bases Aerodynamic configurations Computational fluid dynamics Wind tunnel test Index. décimale : 363.124 Risques dans les transports : Transports aérien et spatial Résumé : This report presents the results of a study by Working Group 14 of the AGARD Fluid Dynamics Panel. This group was formed to establish an accessible, detailed experimental data base for the validation of Fluid Dynamics (CFD) codes.
The thirty nine test cases are documented cover the subsonic, transonic; and supersonic flow regimes and five classes of geometries. Included in the five classes of geometries are: Two Dimensional Airfoils; Three Dimensional Wings, designed for predominantly attached flow conditions; Slender Bodies, typical of missile type configurations; Delta Wings, characterized by a conical type of vortex flow; and Complex Configurations, either in a geometrical sense or because of complicated flow onteractions.Exemplaires
Code-barres Cote Support Localisation Section Disponibilité 3133 8-AR 363.124 AGA Ouvrages Bibliothèque d'archives de l'Académie AR - Donation MAREC Jean-Pierre Archives AAE-Donations
Exclu du prêtRTO Technical Report, n°27. A feasibility study of collaborative muti-facility windtunnel testing for CFD validation / RTO Applied Vehicule Technology (AVT) (1999) / 978-92-8371-023-3
Titre de série : RTO Technical Report, n°27 Titre : A feasibility study of collaborative muti-facility windtunnel testing for CFD validation : Report of the RTO Applied Vehicule Technology panel (AVT) working group 011 Titre original : Etude de faisabilité d'essais en soufflerie multisites menés en coopération, en vue de la validation des calculs de l'aérodynamique numérique -CFD 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-TR-27 Importance : 29 pages Présentation : ill. noir&blanc, schémas, photos Format : 29.5 x 21 cm ISBN/ISSN/EAN : 978-92-8371-023-3 Langues : Anglais (eng) Catégories : Thésaurus AAE
Aéronautique (Ouvrages Généraux):Génie aéronautique:AérodynamiqueTags : wind tunnel tests wind tunnels computational fluid dynamics international cooperation algorithms experimental data computation comparison validity fighter aircraft transport aircraft rotary wing aircraft helicopters missiles flow distribution flow measurement test facilities cost effectiveness Index. décimale : D.001.3 Aérodynamique Résumé : The working group, after an initial enquiry, established the need for CFD validation for fighter aircraft, transport type aircraft, missiles and helicopters. Effort and cost can be controlled efficiently and would permit the improvementof CFD codes for considerable costsaving in futur development RTO Technical Report, n°27. A feasibility study of collaborative muti-facility windtunnel testing for CFD validation = Etude de faisabilité d'essais en soufflerie multisites menés en coopération, en vue de la validation des calculs de l'aérodynamique numérique -CFD : Report of the RTO Applied Vehicule Technology panel (AVT) working group 011 [texte imprimé] / RTO Applied Vehicule Technology (AVT), Auteur . - [S.l.] : NATO - OTAN, 1999 . - 29 pages : ill. noir&blanc, schémas, photos ; 29.5 x 21 cm. - (RTO Research and Technology Organisation; RTO-TR-27) .
ISBN : 978-92-8371-023-3
Langues : Anglais (eng)
Catégories : Thésaurus AAE
Aéronautique (Ouvrages Généraux):Génie aéronautique:AérodynamiqueTags : wind tunnel tests wind tunnels computational fluid dynamics international cooperation algorithms experimental data computation comparison validity fighter aircraft transport aircraft rotary wing aircraft helicopters missiles flow distribution flow measurement test facilities cost effectiveness Index. décimale : D.001.3 Aérodynamique Résumé : The working group, after an initial enquiry, established the need for CFD validation for fighter aircraft, transport type aircraft, missiles and helicopters. Effort and cost can be controlled efficiently and would permit the improvementof CFD codes for considerable costsaving in futur development Réservation
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Code-barres Cote Support Localisation Section Disponibilité 241 D.001.3 RTO Ouvrages Centre de documentation Collection OTAN - NATO Disponible
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