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AGARD Advisory Report. Identification of dynamic systems - Applications to aircraft part 1 : The output error Approach / AGARD Flight (1986)
Titre de série : AGARD Advisory Report Titre : Identification of dynamic systems - Applications to aircraft part 1 : The output error Approach Type de document : texte imprimé Auteurs : AGARD Flight, Auteur Editeur : NATO - OTAN Année de publication : 1986 Collection : AGARD - Advisory Group for Aerospace Research and Development num. AGARD-AR-300 Volume 3 Part 1 Importance : 184 p. Format : 21 x 30 cm. Langues : Anglais (eng) Catégories : Archives
8 AR-P.MARETags : Aerodynamic stability Flight control Flight characteristics Flight maneuvers Flight test Data processing Index. décimale : 363.124 Risques dans les transports : Transports aérien et spatial Résumé : This document examines the practical application of parameter estimation methodology to the problem of estimating aircraft stability and control derivatives from flight test data. The primary purpose of the document is to present a comprehensive and unified picture of the entire parameter estimation process and its integration into a flight test program. The document concentrates on the output-error method to provide a focus for detailed examination and to allow us to give specific examples of situations that have arisen in our experience. AGARD Advisory Report. Identification of dynamic systems - Applications to aircraft part 1 : The output error Approach [texte imprimé] / AGARD Flight, Auteur . - [S.l.] : NATO - OTAN, 1986 . - 184 p. ; 21 x 30 cm.. - (AGARD - Advisory Group for Aerospace Research and Development; AGARD-AR-300 Volume 3 Part 1) .
Langues : Anglais (eng)
Catégories : Archives
8 AR-P.MARETags : Aerodynamic stability Flight control Flight characteristics Flight maneuvers Flight test Data processing Index. décimale : 363.124 Risques dans les transports : Transports aérien et spatial Résumé : This document examines the practical application of parameter estimation methodology to the problem of estimating aircraft stability and control derivatives from flight test data. The primary purpose of the document is to present a comprehensive and unified picture of the entire parameter estimation process and its integration into a flight test program. The document concentrates on the output-error method to provide a focus for detailed examination and to allow us to give specific examples of situations that have arisen in our experience. Exemplaires
Code-barres Cote Support Localisation Section Disponibilité 3168 8-AR 363.124 AGA Ouvrages Bibliothèque d'archives de l'Académie AR - Donation MAREC Jean-Pierre Archives AAE-Donations
Exclu du prêtAGARD Advisory Group. Rotorcraft system identification / AGARD Lecture Series (1991) / 978-92-8350-640-9
Titre de série : AGARD Advisory Group Titre : Rotorcraft system identification Type de document : texte imprimé Auteurs : AGARD Lecture Series, Auteur Editeur : NATO - OTAN Année de publication : 1991 Collection : AGARD - Advisory Group for Aerospace Research and Development num. AGARD-LS-178 Importance : 258 p. Format : 21 x 30 cm. ISBN/ISSN/EAN : 978-92-8350-640-9 Langues : Anglais (eng) Catégories : Archives
8 AR-P.MARETags : Rotary wing aircraft Flight tests Aerodynamic stability Proving Identifying Mathematical models helicopters Index. décimale : 363.124 Risques dans les transports : Transports aérien et spatial Résumé : For fixed wing aircraft, system identification methods to determine stability and control derivatives from flight test data used with confidence. The application of the same techniques to rotorcraft is not so far advanced mainly because of the helicopter aeromechanical complexity. Only a few specialists; mostly in research organisations, have concentrated on this field and the application in industry is still sporadic. AGARD Advisory Group. Rotorcraft system identification [texte imprimé] / AGARD Lecture Series, Auteur . - [S.l.] : NATO - OTAN, 1991 . - 258 p. ; 21 x 30 cm.. - (AGARD - Advisory Group for Aerospace Research and Development; AGARD-LS-178) .
ISBN : 978-92-8350-640-9
Langues : Anglais (eng)
Catégories : Archives
8 AR-P.MARETags : Rotary wing aircraft Flight tests Aerodynamic stability Proving Identifying Mathematical models helicopters Index. décimale : 363.124 Risques dans les transports : Transports aérien et spatial Résumé : For fixed wing aircraft, system identification methods to determine stability and control derivatives from flight test data used with confidence. The application of the same techniques to rotorcraft is not so far advanced mainly because of the helicopter aeromechanical complexity. Only a few specialists; mostly in research organisations, have concentrated on this field and the application in industry is still sporadic. Exemplaires
Code-barres Cote Support Localisation Section Disponibilité 3192 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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Code-barres Cote Support Localisation Section Disponibilité 213 D.001.3 AGA Ouvrages Centre de documentation Collection OTAN - NATO Disponible Reports on wind tunnel experiments in aerodynamics / Jerome C. Hunsaker (1916)
Titre : Reports on wind tunnel experiments in aerodynamics : (with five plates) Type de document : texte imprimé Auteurs : Jerome C. Hunsaker, Auteur Editeur : Washington : Smithsonian Institution Année de publication : 1916 Importance : 92p. Format : 24,5 cm Langues : Français (fre) Catégories : Thésaurus AAE
Aéronautique (Ouvrages Généraux)Tags : aerodynamic experiment theory stability dirigible Index. décimale : 629.132 3 Génie aéronautique : Aérodynamique Reports on wind tunnel experiments in aerodynamics : (with five plates) [texte imprimé] / Jerome C. Hunsaker, Auteur . - Washington : Smithsonian Institution, 1916 . - 92p. ; 24,5 cm.
Langues : Français (fre)
Catégories : Thésaurus AAE
Aéronautique (Ouvrages Généraux)Tags : aerodynamic experiment theory stability dirigible Index. décimale : 629.132 3 Génie aéronautique : Aérodynamique Réservation
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Code-barres Cote Support Localisation Section Disponibilité 1219 629.132 3 HUN Rapports Centre de documentation Bibliothèque AAE Disponible 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. Developmental airdrop testing techniques and devices / AGARD Flight (1987) / 978-92-8351-559-3
PermalinkAGARD Advisory Report. Enhancement of Aircraft Ground Handling Simulation Capability / AGARD Flight (1998)
PermalinkAGARD Advisory Report. Identification of dynamic systems - Applications to aircraft part 2 : Nonlinear analysis and manoeuvre design. / AGARD Flight (1994)
PermalinkAGARD Advisory Report. Manual on the Flight of flexible aircraft in turbulence / AGARD Flight (1991)
PermalinkAGARD Advisory Report. Rotary balance testing for aircraft dynamics / AGARD Advisory Group (1990)
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