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
19 résultat(s) recherche sur le tag 'aerodynamic configurations'
Affiner la recherche
AGARD Advisory Report. Aerodynamics of aircraft afterbody / AGARD Advisory Group (1986)
Titre de série : AGARD Advisory Report Titre : Aerodynamics of aircraft afterbody Type de document : texte imprimé Auteurs : AGARD Advisory Group, Auteur Editeur : NATO - OTAN Année de publication : 1986 Collection : AGARD - Advisory Group for Aerospace Research and Development num. AGARD-AR-226 Importance : 348 p. Format : 21 x 30 cm. Langues : Anglais (eng) Catégories : Archives
8 AR-P.MARETags : Aerodynamic configurations Aerodynamic characteristics, Afterbodies Drag Fighter aircraft Index. décimale : 363.124 Risques dans les transports : Transports aérien et spatial Résumé : Aircraft afterbody design is still one of the most critical problems for industry, especially in fighter aircraft development. The flow around the rear part of the fuselage is characterized by the simultaneous occurence of interfering physical phenomena such as thick turbulent boundary layers, viscious flow separation, hot jet interference at the base and the boat tail, and jet plume expansion in three_dimensional transonic and supersonic flow. Even experimental techniques hardly fulfill requirements for correct wind tunnel simulation of all effects. Note de contenu : appendix : experimentation data base AGARD Advisory Report. Aerodynamics of aircraft afterbody [texte imprimé] / AGARD Advisory Group, Auteur . - [S.l.] : NATO - OTAN, 1986 . - 348 p. ; 21 x 30 cm.. - (AGARD - Advisory Group for Aerospace Research and Development; AGARD-AR-226) .
Langues : Anglais (eng)
Catégories : Archives
8 AR-P.MARETags : Aerodynamic configurations Aerodynamic characteristics, Afterbodies Drag Fighter aircraft Index. décimale : 363.124 Risques dans les transports : Transports aérien et spatial Résumé : Aircraft afterbody design is still one of the most critical problems for industry, especially in fighter aircraft development. The flow around the rear part of the fuselage is characterized by the simultaneous occurence of interfering physical phenomena such as thick turbulent boundary layers, viscious flow separation, hot jet interference at the base and the boat tail, and jet plume expansion in three_dimensional transonic and supersonic flow. Even experimental techniques hardly fulfill requirements for correct wind tunnel simulation of all effects. Note de contenu : appendix : experimentation data base Exemplaires
Code-barres Cote Support Localisation Section Disponibilité 3140 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 prêtAGARD Report, n°776. Special course on aircraft aerodynamics at high angles of attacks : experiments and modelling / AGARD Fluid Dynamics Panel (1991) / 978-92-8350-607-2
Titre de série : AGARD Report, n°776 Titre : Special course on aircraft aerodynamics at high angles of attacks : experiments and modelling : NASA Langley Research Center, Hampton, Virginia 23665, United States,8th to 11th april 1991 and the von Karman Institut, Rhode-Saint-Genèse, Belgium, 22nd to 25th april 1991 Titre original : La dynamique de vol des aéronefs aux grands angles d'attaque : expérimentation et modélisation Type de document : texte imprimé Auteurs : AGARD Fluid Dynamics Panel, Auteur Editeur : NATO - OTAN Année de publication : 1991 Collection : AGARD - Advisory Group for Aerospace Research and Development num. AGARD-R-776 Importance : pagination multiple Présentation : ill. noir&blanc, schémas, photos Format : 29,5 x 21 cm ISBN/ISSN/EAN : 978-92-8350-607-2 Prix : Distribution of Unclassified AGARD Publications Langues : Anglais (eng) Catégories : Thésaurus AAE
Aéronautique (Ouvrages Généraux)Tags : wind tunnels lift vortices aerodynamic configurations aircraft fluid dynamics mathematical models flight tests flight characteristics aerodynamic characteristics fluid flow aerodynamic stability aerofoils Index. décimale : D.001.3 Aérodynamique Résumé : These note provide the latest information on the development and use of dynamic experiments in wind tunnels from several of the NATO nations. AGARD Report, n°776. Special course on aircraft aerodynamics at high angles of attacks : experiments and modelling = La dynamique de vol des aéronefs aux grands angles d'attaque : expérimentation et modélisation : NASA Langley Research Center, Hampton, Virginia 23665, United States,8th to 11th april 1991 and the von Karman Institut, Rhode-Saint-Genèse, Belgium, 22nd to 25th april 1991 [texte imprimé] / AGARD Fluid Dynamics Panel, Auteur . - [S.l.] : NATO - OTAN, 1991 . - pagination multiple : ill. noir&blanc, schémas, photos ; 29,5 x 21 cm. - (AGARD - Advisory Group for Aerospace Research and Development; AGARD-R-776) .
ISBN : 978-92-8350-607-2 : Distribution of Unclassified AGARD Publications
Langues : Anglais (eng)
Catégories : Thésaurus AAE
Aéronautique (Ouvrages Généraux)Tags : wind tunnels lift vortices aerodynamic configurations aircraft fluid dynamics mathematical models flight tests flight characteristics aerodynamic characteristics fluid flow aerodynamic stability aerofoils Index. décimale : D.001.3 Aérodynamique Résumé : These note provide the latest information on the development and use of dynamic experiments in wind tunnels from several of the NATO nations. Réservation
Réserver ce document
Exemplaires
Code-barres Cote Support Localisation Section Disponibilité 213 D.001.3 AGA Ouvrages Centre de documentation Collection OTAN - NATO Disponible RTO Meeting proceedings, 35. Aerodynamic design and optimisation of flight vehicles in a concurrent multidisciplinary environment / RTO Applied Vehicule Technology (AVT) (2000) / 978-92-8371-040-0
Titre de série : RTO Meeting proceedings, 35 Titre : Aerodynamic design and optimisation of flight vehicles in a concurrent multidisciplinary environment : Papers presented at the specialists Meeting of the RTO Applied Vehicle Technology Panel (AVT), held in Corfu, Greece, 21-22 april 1999 Titre original : La conception et l'optimisation aérodynamique des véhicules aériens dans un environnement pluridisciplinaire et simultané Type de document : texte imprimé Auteurs : RTO Applied Vehicule Technology (AVT), Auteur Editeur : NATO - OTAN Année de publication : 2000 Collection : RTO Research and Technology Organisation num. RTO-MP-35 AC/323/(AVT)TP/15 Importance : pagination multiple Présentation : ill. noir&blanc, couleurs, schémas, photos Format : 29.5 x 21 cm ISBN/ISSN/EAN : 978-92-8371-040-0 Prix : Distribution of Unclassified RTO Publications Langues : Anglais (eng) Catégories : Thésaurus AAE
Aéronautique (Ouvrages Généraux):Génie aéronautique:AérodynamiqueTags : aerodynamics design NATO international cooperation optimization aerospace engineering aerodynamic configurations military aircraft high lift devices fluid dynamics wings airfoils computer aided design missiles data bases data processing MDO (Multidisciplinary Design Optimization),procurement tools rapid design system aerospace craft military operations requirements Index. décimale : D.001.3 Aérodynamique Résumé : The symposium dealt with design and more specifically aerodynamic design and optimisatin of flight vehicles in a concurrent multi-disciplinary environment. RTO Meeting proceedings, 35. Aerodynamic design and optimisation of flight vehicles in a concurrent multidisciplinary environment = La conception et l'optimisation aérodynamique des véhicules aériens dans un environnement pluridisciplinaire et simultané : Papers presented at the specialists Meeting of the RTO Applied Vehicle Technology Panel (AVT), held in Corfu, Greece, 21-22 april 1999 [texte imprimé] / RTO Applied Vehicule Technology (AVT), Auteur . - [S.l.] : NATO - OTAN, 2000 . - pagination multiple : ill. noir&blanc, couleurs, schémas, photos ; 29.5 x 21 cm. - (RTO Research and Technology Organisation; RTO-MP-35 AC/323/(AVT)TP/15) .
ISBN : 978-92-8371-040-0 : Distribution of Unclassified RTO Publications
Langues : Anglais (eng)
Catégories : Thésaurus AAE
Aéronautique (Ouvrages Généraux):Génie aéronautique:AérodynamiqueTags : aerodynamics design NATO international cooperation optimization aerospace engineering aerodynamic configurations military aircraft high lift devices fluid dynamics wings airfoils computer aided design missiles data bases data processing MDO (Multidisciplinary Design Optimization),procurement tools rapid design system aerospace craft military operations requirements Index. décimale : D.001.3 Aérodynamique Résumé : The symposium dealt with design and more specifically aerodynamic design and optimisatin of flight vehicles in a concurrent multi-disciplinary environment. Réservation
Réserver ce document
Exemplaires
Code-barres Cote Support Localisation Section Disponibilité 236 D.001.3 RTO Ouvrages Centre de documentation Collection OTAN - NATO Disponible RTO Meeting proceedings, 45. Search and target acquisition / RTO Systems Concepts and Integrations panel (SCI) (2000) / 978-92-8371-035-6
PermalinkAGARD Advisory Group. Rotorcraft system identification / AGARD Lecture Series (1991) / 978-92-8350-640-9
PermalinkAGARD Advisory Report. Developmental airdrop testing techniques and devices / AGARD Flight (1987) / 978-92-8351-559-3
PermalinkAGARD Advisory Report. Identification of dynamic systems - Applications to aircraft part 1 : The output error Approach / AGARD Flight (1986)
PermalinkAGARD Advisory Report. Manual on the Flight of flexible aircraft in turbulence / AGARD Flight (1991)
Permalink
Recherches dans d'autres bibliothèques et centres de ressources : |
||
AAE
pmb