Flapping wings became a primary source of inspiration for research into Micro Air Vehicles (MAVs), Unmanned Aerial Vehicles (UAVs) etc. For practical applications, the flapping wing has to adapt the morphology and kinematics that match the dynamical features of fluids to attain efficient propulsion. The book describes numerical investigations on a teardrop-shaped airfoil and wing performing different flapping oscillations. Pitching, heaving and the combined motion of pitch and heave are the different flapping oscillations investigated. A uniform, laminar, incompressible flow is considered over the airfoil and wing while performing the flapping oscillations. The influence of flapping frequency and amplitude on the wake characteristics behind the flapping airfoil are discussed. The force experienced by the flapping wing depends on the vortex structures and their evolution. The identification of vortex formation, their interactions and separation from the wing surface are necessary to understand the force experienced by the wing. The influence of aspect ratio on the formation and evolution of vortex structures is relevant in developing practical applications.
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Vendeur : BuchWeltWeit Ludwig Meier e.K., Bergisch Gladbach, Allemagne
Taschenbuch. Etat : Neu. This item is printed on demand - it takes 3-4 days longer - Neuware -Flapping wings became a primary source of inspiration for research into Micro Air Vehicles (MAVs), Unmanned Aerial Vehicles (UAVs) etc. For practical applications, the flapping wing has to adapt the morphology and kinematics that match the dynamical features of fluids to attain efficient propulsion. The book describes numerical investigations on a teardrop-shaped airfoil and wing performing different flapping oscillations. Pitching, heaving and the combined motion of pitch and heave are the different flapping oscillations investigated. A uniform, laminar, incompressible flow is considered over the airfoil and wing while performing the flapping oscillations. The influence of flapping frequency and amplitude on the wake characteristics behind the flapping airfoil are discussed. The force experienced by the flapping wing depends on the vortex structures and their evolution. The identification of vortex formation, their interactions and separation from the wing surface are necessary to understand the force experienced by the wing. The influence of aspect ratio on the formation and evolution of vortex structures is relevant in developing practical applications. 156 pp. Englisch. N° de réf. du vendeur 9786206144243
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Vendeur : moluna, Greven, Allemagne
Kartoniert / Broschiert. Etat : New. Dieser Artikel ist ein Print on Demand Artikel und wird nach Ihrer Bestellung fuer Sie gedruckt. Flapping wings became a primary source of inspiration for research into Micro Air Vehicles (MAVs), Unmanned Aerial Vehicles (UAVs) etc. For practical applications, the flapping wing has to adapt the morphology and kinematics that match the dynamical feature. N° de réf. du vendeur 830796227
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Vendeur : preigu, Osnabrück, Allemagne
Taschenbuch. Etat : Neu. Flapping Wings: Bio-mimicking for future | A computational perspective of applications | V K Vineeth (u. a.) | Taschenbuch | Englisch | 2023 | LAP LAMBERT Academic Publishing | EAN 9786206144243 | Verantwortliche Person für die EU: preigu GmbH & Co. KG, Lengericher Landstr. 19, 49078 Osnabrück, mail[at]preigu[dot]de | Anbieter: preigu. N° de réf. du vendeur 126677700
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Vendeur : buchversandmimpf2000, Emtmannsberg, BAYE, Allemagne
Taschenbuch. Etat : Neu. This item is printed on demand - Print on Demand Titel. Neuware -Flapping wings became a primary source of inspiration for research into Micro Air Vehicles (MAVs), Unmanned Aerial Vehicles (UAVs) etc. For practical applications, the flapping wing has to adapt the morphology and kinematics that match the dynamical features of fluids to attain efficient propulsion. The book describes numerical investigations on a teardrop-shaped airfoil and wing performing different flapping oscillations. Pitching, heaving and the combined motion of pitch and heave are the different flapping oscillations investigated. A uniform, laminar, incompressible flow is considered over the airfoil and wing while performing the flapping oscillations. The influence of flapping frequency and amplitude on the wake characteristics behind the flapping airfoil are discussed. The force experienced by the flapping wing depends on the vortex structures and their evolution. The identification of vortex formation, their interactions and separation from the wing surface are necessary to understand the force experienced by the wing. The influence of aspect ratio on the formation and evolution of vortex structures is relevant in developing practical applications.VDM Verlag, Dudweiler Landstraße 99, 66123 Saarbrücken 156 pp. Englisch. N° de réf. du vendeur 9786206144243
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Vendeur : AHA-BUCH GmbH, Einbeck, Allemagne
Taschenbuch. Etat : Neu. nach der Bestellung gedruckt Neuware - Printed after ordering - Flapping wings became a primary source of inspiration for research into Micro Air Vehicles (MAVs), Unmanned Aerial Vehicles (UAVs) etc. For practical applications, the flapping wing has to adapt the morphology and kinematics that match the dynamical features of fluids to attain efficient propulsion. The book describes numerical investigations on a teardrop-shaped airfoil and wing performing different flapping oscillations. Pitching, heaving and the combined motion of pitch and heave are the different flapping oscillations investigated. A uniform, laminar, incompressible flow is considered over the airfoil and wing while performing the flapping oscillations. The influence of flapping frequency and amplitude on the wake characteristics behind the flapping airfoil are discussed. The force experienced by the flapping wing depends on the vortex structures and their evolution. The identification of vortex formation, their interactions and separation from the wing surface are necessary to understand the force experienced by the wing. The influence of aspect ratio on the formation and evolution of vortex structures is relevant in developing practical applications. N° de réf. du vendeur 9786206144243
Quantité disponible : 1 disponible(s)