Suday k ghosh (2 risultati)

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    • Lingua: Inglese

      Editore: VDM Verlag Dr. Müller, 2010

      3639288947 / 9783639288940

      • Brossura

      Da: preigu, Osnabrück, Germaniapreigu

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      Condizione: Nuovo

      EUR 66,50

      EUR 70,00 spedizione 
      Spedito da Germania a U.S.A.

      Quantità: 5 disponibili

      Taschenbuch. Condizione: Neu. Incompressible Boundary Layer Control for Flow Past Circular Cylinder | Numerical Study | Suday K. Ghosh | Taschenbuch | Englisch | VDM Verlag Dr. Müller | EAN 9783639288940 | Verantwortliche Person für die EU: preigu GmbH & Co. KG, Lengericher Landstr. 19, 49078 Osnabrück, mail[at]preigu[dot]de | Anbieter: preigu.

    • Lingua: Inglese

      Editore: VDM Verlag Dr. Müller, 2010

      3639288947 / 9783639288940

      • Brossura
      • Print on Demand

      Da: AHA-BUCH GmbH, Einbeck, GermaniaAHA-BUCH GmbH

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      Condizione: Nuovo

      EUR 79,95

      EUR 62,20 spedizione 
      Spedito da Germania a U.S.A.

      Quantità: 2 disponibili

      Taschenbuch. Condizione: Neu. nach der Bestellung gedruckt Neuware - Printed after ordering - Present work investigates effects of application of different boundary layer control mechanisms on 2-D incompressible laminar flow around circular cylinder at different ow conditions. It focuses unsteady cases with its transient conditions. Unsteady Navier-Stokes equations are deployed. In tangential blowing from cylinder surface, both point blowing and span blowing are considered to study variations of lift, drag by varying blowing port positions and intensity of blowing. Effects on unsteadiness are also examined. In case of rotation of cylinder surface for controlling boundary layer, lift and drag are inves tigated by varying rotational speeds. Rotation has been found to have strong in uence on ow and mode of vortex shedding gets changed from the surface. Rotational oscillation of cylinder surface, both for Lock-on and non-Lock-on cases have been studied. Frequency and amplitude of rotational oscillation are made to vary to investigate effects on the lift and drag. It reveals that the effect of amplitude of oscillation on drag is complicated and ratio of forcing frequency and natural frequency affects ow conditions substantially.