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AGARD Advisory Group. Advanced Aerodynamic Measurement Technology / AGARD Conférence Proceeding (1998)
Titre de série : AGARD Advisory Group Titre : Advanced Aerodynamic Measurement Technology Type de document : texte imprimé Auteurs : AGARD Conférence Proceeding, Auteur Editeur : NATO - OTAN Année de publication : 1998 Collection : AGARD - Advisory Group for Aerospace Research and Development num. AGARD-CP-601 Importance : 420 p. Format : 21 x 30 cm. Langues : Anglais (eng) Catégories : Archives
8 AR-P.MARETags : wind tunnels Measurement Measuring instruments Flow visualization Velocity measurement Diagnostic equipment Holography Interferometers Flow distribution Fluid dynamics Index. décimale : 363.124 Risques dans les transports : Transports aérien et spatial Résumé : The papers prepared for the AGARD Fluid dynamic Panel (FDP) Symposium on "Advanced Aerodynamic Measurement Technology" which was held 22-25 September, 1997 in Seattle, Washington, USA, are contained in this Report. In addition, a Technical Evaluator's Report aimed at assessing the success of the Symposium in meeting its objectives, and an edited transcript of the General Discussion held at the end of the Symposium are also inclued.
AGARD Advisory Group. Advanced Aerodynamic Measurement Technology [texte imprimé] / AGARD Conférence Proceeding, Auteur . - [S.l.] : NATO - OTAN, 1998 . - 420 p. ; 21 x 30 cm.. - (AGARD - Advisory Group for Aerospace Research and Development; AGARD-CP-601) .
Langues : Anglais (eng)
Catégories : Archives
8 AR-P.MARETags : wind tunnels Measurement Measuring instruments Flow visualization Velocity measurement Diagnostic equipment Holography Interferometers Flow distribution Fluid dynamics Index. décimale : 363.124 Risques dans les transports : Transports aérien et spatial Résumé : The papers prepared for the AGARD Fluid dynamic Panel (FDP) Symposium on "Advanced Aerodynamic Measurement Technology" which was held 22-25 September, 1997 in Seattle, Washington, USA, are contained in this Report. In addition, a Technical Evaluator's Report aimed at assessing the success of the Symposium in meeting its objectives, and an edited transcript of the General Discussion held at the end of the Symposium are also inclued.
Exemplaires
Code-barres Cote Support Localisation Section Disponibilité 3283 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 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
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Exemplaires
Code-barres Cote Support Localisation Section Disponibilité 213 D.001.3 AGA Ouvrages Centre de documentation Collection OTAN - NATO Disponible 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 Group, 197. Flight in an adverse environment / AGARD Lecture Series (1994) / 978-92-8361-006-9
Titre de série : AGARD Advisory Group, 197 Titre : Flight in an adverse environment Titre original : Le vol en environnement hostile Type de document : texte imprimé Auteurs : AGARD Lecture Series, Auteur Editeur : NATO - OTAN Année de publication : 1994 Collection : AGARD - Advisory Group for Aerospace Research and Development num. AGARD-LS-197 Importance : 168 p. Présentation : ill. noir&blanc, schémas, photos Format : 30 x 21 cm ISBN/ISSN/EAN : 978-92-8361-006-9 Note générale : This publication was prepared at the request of the Flight Vehicle Integration Panel and under the sponsorship ot the consultant and exchange programme of AGARD and will be presented on 7-8 november 1994 in Braunschweig, Germany, 10-11 november in Lisbon, Portugal, and 15-16 november 1994 in Atlantic city, USA Langues : Anglais (eng) Catégories : Archives
8 AR-P.MARETags : aviation safety aircraft flight flight tests turbulence wakes wind shear gusts storms rain icing lightning electromagnetic environments adverse conditions Index. décimale : 363.124 Risques dans les transports : Transports aérien et spatial Résumé : The environment in which an airplane must operate is a major cause of aircraft accidents. This lecture series focuses on specific aspects of the environment, both natural and man-made, which are the major contributors to these accidents as follows. AGARD Advisory Group, 197. Flight in an adverse environment = Le vol en environnement hostile [texte imprimé] / AGARD Lecture Series, Auteur . - [S.l.] : NATO - OTAN, 1994 . - 168 p. : ill. noir&blanc, schémas, photos ; 30 x 21 cm. - (AGARD - Advisory Group for Aerospace Research and Development; AGARD-LS-197) .
ISBN : 978-92-8361-006-9
This publication was prepared at the request of the Flight Vehicle Integration Panel and under the sponsorship ot the consultant and exchange programme of AGARD and will be presented on 7-8 november 1994 in Braunschweig, Germany, 10-11 november in Lisbon, Portugal, and 15-16 november 1994 in Atlantic city, USA
Langues : Anglais (eng)
Catégories : Archives
8 AR-P.MARETags : aviation safety aircraft flight flight tests turbulence wakes wind shear gusts storms rain icing lightning electromagnetic environments adverse conditions Index. décimale : 363.124 Risques dans les transports : Transports aérien et spatial Résumé : The environment in which an airplane must operate is a major cause of aircraft accidents. This lecture series focuses on specific aspects of the environment, both natural and man-made, which are the major contributors to these accidents as follows. Exemplaires
Code-barres Cote Support Localisation Section Disponibilité 202 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. Aircraft Trajectories - Computation - Prediction - Control Volume 1 / AGARD Flight (1990)
PermalinkAGARD Advisory Report. A selection of Experimental Test Cases for the Validation of CFD Codes / AGARD Advisory Group (1994) / 978-92-8361-002-1
PermalinkAGARD Advisory Report. A selection of Experimental Test Cases for the Validation of CFD Codes / AGARD Advisory Group (1994)
PermalinkAGARDograph, n°301. Aircraft trajectories computation - prediction - control volume 1 / AGARD Guidance and Control panel (1990) / 978-92-8350-547-1
PermalinkRTO Meeting proceedings, 16. Aircraft weapon system compatibility and integration / RTO Systems Concepts and Integrations panel (SCI) (1999) / 978-92-8370-007-4
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