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RTO 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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Exemplaires
Code-barres Cote Support Localisation Section Disponibilité 241 D.001.3 RTO Ouvrages Centre de documentation Collection OTAN - NATO Disponible AGARD 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 prêtAGARD Advisory Report. Sonic Nozzles for Mass Flow Measurement and Reference Nozzle for thrust Verification / AGARD Advisory Group (1997) / 978-92-8361-056-4
Titre de série : AGARD Advisory Report Titre : Sonic Nozzles for Mass Flow Measurement and Reference Nozzle for thrust Verification Type de document : texte imprimé Auteurs : AGARD Advisory Group, Auteur Editeur : NATO - OTAN Année de publication : 1997 Collection : AGARD - Advisory Group for Aerospace Research and Development num. AGARD-AR-321 Importance : 84 p. Présentation : schémas Format : 21 x 30 cm. ISBN/ISSN/EAN : 978-92-8361-056-4 Langues : Anglais (eng) Catégories : Archives
8 AR-P.MARETags : Wind tunnels Mass flowmeters Drag Calibrating Transferring Standards Test Nozzles Aircraft engines Viscosity Thrust meters Index. décimale : 363.124 Risques dans les transports : Transports aérien et spatial Résumé : This report presents the results of a multinational effort to reflect the state-of-the Art for the accurate measurement of massflow and thrust. The accurate measurements of these quantities is essential to the success of windtunnel tests supporting engine-airframe aerodynamic integration studies. Ist is concluded that the measurement og gaseous mass flows with +0.1% respectively. For thrust measurements, these values must typically be doubled. AGARD Advisory Report. Sonic Nozzles for Mass Flow Measurement and Reference Nozzle for thrust Verification [texte imprimé] / AGARD Advisory Group, Auteur . - [S.l.] : NATO - OTAN, 1997 . - 84 p. : schémas ; 21 x 30 cm.. - (AGARD - Advisory Group for Aerospace Research and Development; AGARD-AR-321) .
ISBN : 978-92-8361-056-4
Langues : Anglais (eng)
Catégories : Archives
8 AR-P.MARETags : Wind tunnels Mass flowmeters Drag Calibrating Transferring Standards Test Nozzles Aircraft engines Viscosity Thrust meters Index. décimale : 363.124 Risques dans les transports : Transports aérien et spatial Résumé : This report presents the results of a multinational effort to reflect the state-of-the Art for the accurate measurement of massflow and thrust. The accurate measurements of these quantities is essential to the success of windtunnel tests supporting engine-airframe aerodynamic integration studies. Ist is concluded that the measurement og gaseous mass flows with +0.1% respectively. For thrust measurements, these values must typically be doubled. Exemplaires
Code-barres Cote Support Localisation Section Disponibilité 2907 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, 16. Aircraft weapon system compatibility and integration / RTO Systems Concepts and Integrations panel (SCI) (1999) / 978-92-8370-007-4
Titre de série : RTO Meeting proceedings, 16 Titre : Aircraft weapon system compatibility and integration : Papers presented at the Systems Concepts and Integration Panel (SCI) symposium held in Chester, United Kingdom, 28-30 september 1998 Titre original : Compatibilité et intégration des systèmes d'armes aéroportés Type de document : texte imprimé Auteurs : RTO Systems Concepts and Integrations panel (SCI), Auteur Editeur : NATO - OTAN Année de publication : 1999 Collection : RTO Research and Technology Organisation num. RTO-MP-16 AC/323/(SCI)TP/8 Importance : pagination multiple Présentation : ill. noir&blanc, couleurs, schémas, photos Format : 29.5 x 21 cm ISBN/ISSN/EAN : 978-92-8370-007-4 Prix : Distribution of Unclassified RTO Publications Langues : Anglais (eng) Catégories : Thésaurus AAE
Armée (Ouvrages Généraux):Aéronef militaireTags : weapons systems military aircraft integrated systems compatibility flight tests computational fluid dynamics wind tunnel tests external stores trajectories mathematical models computerized simulation separation structural analysis aerodynamics aerodynamic loads Index. décimale : C.001 Aéronef militaire Résumé : Economic constraints dictate that the lives of existing aircraft must be stretched, making the incorporation of new weapons and weapon systems into existing airframes necessary RTO Meeting proceedings, 16. Aircraft weapon system compatibility and integration = Compatibilité et intégration des systèmes d'armes aéroportés : Papers presented at the Systems Concepts and Integration Panel (SCI) symposium held in Chester, United Kingdom, 28-30 september 1998 [texte imprimé] / RTO Systems Concepts and Integrations panel (SCI), Auteur . - [S.l.] : NATO - OTAN, 1999 . - pagination multiple : ill. noir&blanc, couleurs, schémas, photos ; 29.5 x 21 cm. - (RTO Research and Technology Organisation; RTO-MP-16 AC/323/(SCI)TP/8) .
ISBN : 978-92-8370-007-4 : Distribution of Unclassified RTO Publications
Langues : Anglais (eng)
Catégories : Thésaurus AAE
Armée (Ouvrages Généraux):Aéronef militaireTags : weapons systems military aircraft integrated systems compatibility flight tests computational fluid dynamics wind tunnel tests external stores trajectories mathematical models computerized simulation separation structural analysis aerodynamics aerodynamic loads Index. décimale : C.001 Aéronef militaire Résumé : Economic constraints dictate that the lives of existing aircraft must be stretched, making the incorporation of new weapons and weapon systems into existing airframes necessary Réservation
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Exemplaires
Code-barres Cote Support Localisation Section Disponibilité 229 C.001 RTO Ouvrages Centre de documentation Collection OTAN - NATO Disponible AGARD Advisory Group, 197. Flight in an adverse environment / AGARD Lecture Series (1994) / 978-92-8361-006-9
PermalinkAGARD Advisory Group, 217. Planar optical measurement methods for gas turbine components / AGARD Lecture Series (1999) / 978-92-8371-019-6
PermalinkAGARD Advisory Group. Advanced Aerodynamic Measurement Technology / AGARD Conférence Proceeding (1998)
PermalinkAGARD Advisory Group. Aerodynamics of wind tunnel circuits and their Components / AGARD Conférence Proceeding (1997) / 978-92-8360-042-8
PermalinkAGARD Advisory Group. Future Aerospace Technology in the Service of the Alliance: Sustained Hypersonic Flight / AGARD Conférence Proceeding (1997)
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