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Auteur E. H. Dowell
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Faire une suggestion Affiner la rechercheA modern course in aeroelasticity / E. H. Dowell
Titre : A modern course in aeroelasticity Type de document : document imprimé Auteurs : E. H. Dowell, Auteur Mention d'édition : 4th rev. and enl. ed. Editeur : Kluwer Academic Publishers Année de publication : 2004 ISBN/ISSN/EAN : 978-1-402-02711-6 Langues : Anglais (eng) A modern course in aeroelasticity [document imprimé] / E. H. Dowell, Auteur . - 4th rev. and enl. ed. . - [S.l.] : Kluwer Academic Publishers, 2004.
ISBN : 978-1-402-02711-6
Langues : Anglais (eng)Réservation
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Code-barres Cote Support Localisation Section Disponibilité CG.2008.049 46 DOW Document imprimé IRPHE Bibliothèque de l'IRPHE Sorti jusqu'au 24/05/2008 AIAA Journal, Vol. 37, n° 3. Limit Cycle Oscillations of a cantilevered Wing in Low Subsonic Flow / Deman Tang
in AIAA journal
Titre de série : AIAA Journal, Vol. 37, n° 3 Titre : Limit Cycle Oscillations of a cantilevered Wing in Low Subsonic Flow Type de document : articles et extraits Auteurs : Deman Tang, Auteur ; Kenneth C. Hall ; E. H. Dowell, Auteur Année de publication : 1999 Importance : pp. 364-371 Langues : Anglais (eng)
in AIAA journal
AIAA Journal, Vol. 37, n° 3. Limit Cycle Oscillations of a cantilevered Wing in Low Subsonic Flow [articles et extraits] / Deman Tang, Auteur ; Kenneth C. Hall ; E. H. Dowell, Auteur . - 1999 . - pp. 364-371.
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Code-barres Cote Support Localisation Section Disponibilité ART-1999364 TAN Document imprimé Bureau chercheur Bureau de ELOY Christophe Disponible AIAA Journal, Vol.5 No.10. Nonlinear Oscillations of a Fluttering Plate. Part. 2 / E. H. Dowell
in AIAA journal
Titre de série : AIAA Journal, Vol.5 No.10 Titre : Nonlinear Oscillations of a Fluttering Plate. Part. 2 Type de document : articles et extraits Auteurs : E. H. Dowell, Auteur Année de publication : 1967 Importance : p.1856-1862 Langues : Français (fre)
in AIAA journal
AIAA Journal, Vol.5 No.10. Nonlinear Oscillations of a Fluttering Plate. Part. 2 [articles et extraits] / E. H. Dowell, Auteur . - 1967 . - p.1856-1862.
Langues : Français (fre)Réservation
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Code-barres Cote Support Localisation Section Disponibilité ART-9435-0 ART Document imprimé Bureau chercheur Bureau de SOUILLIEZ Claire Disponible Journal of sound and vibration, Vol.47 No.2. On the aeroelastic instability of two-dimensional panels in uniform incompressible flow / A. Kornecki
in Journal of sound and vibration
Titre de série : Journal of sound and vibration, Vol.47 No.2 Titre : On the aeroelastic instability of two-dimensional panels in uniform incompressible flow Type de document : articles et extraits Auteurs : A. Kornecki, Auteur ; E. H. Dowell, Auteur ; J. O'Brien, Auteur Année de publication : 1976 Importance : p.163-178 ISBN/ISSN/EAN : 1095-8568 Langues : Français (fre) Résumé : A theoretical and experimental study is presented of the aeroelastic instability of a panel with various boundary conditions on its leading and trailing edges, exposed to air flow over its upper surface or on both sides. The flow is incompressible and two-dimensional (no span-wise deformation of the panel). The case of a panel clamped at its leading edge and free at its trailing edge is investigated both theoretically and experimentally. Agreement between theory and experiment is fair. The aerodynamic theory of steady non-circulatory flow is applied for panels fixed at both ends, and the quasi-steady and full unsteady aerodynamic lifting theories to a cantilevered panel (free at the trailing edge). The analogy with incompressible flow through a long slender tube is pointed out. Theory shows that a panel with both ends fixed loses its stability by divergence, while the instability of a cantilevered panel is of a flutter type. The latter is also confirmed experimentally.
in Journal of sound and vibration
Journal of sound and vibration, Vol.47 No.2. On the aeroelastic instability of two-dimensional panels in uniform incompressible flow [articles et extraits] / A. Kornecki, Auteur ; E. H. Dowell, Auteur ; J. O'Brien, Auteur . - 1976 . - p.163-178.
ISSN : 1095-8568
Langues : Français (fre)
Résumé : A theoretical and experimental study is presented of the aeroelastic instability of a panel with various boundary conditions on its leading and trailing edges, exposed to air flow over its upper surface or on both sides. The flow is incompressible and two-dimensional (no span-wise deformation of the panel). The case of a panel clamped at its leading edge and free at its trailing edge is investigated both theoretically and experimentally. Agreement between theory and experiment is fair. The aerodynamic theory of steady non-circulatory flow is applied for panels fixed at both ends, and the quasi-steady and full unsteady aerodynamic lifting theories to a cantilevered panel (free at the trailing edge). The analogy with incompressible flow through a long slender tube is pointed out. Theory shows that a panel with both ends fixed loses its stability by divergence, while the instability of a cantilevered panel is of a flutter type. The latter is also confirmed experimentally.
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Code-barres Cote Support Localisation Section Disponibilité ART-8464-0 ART Document imprimé Bureau chercheur Bureau de SOUILLIEZ Claire Disponible