Unsteady Compressible Flow over Heaving Bodies Using an Implicit RANS Solver

Siva Kumar , K and Sharanappa, Sajjan V (2011) Unsteady Compressible Flow over Heaving Bodies Using an Implicit RANS Solver. Applied Mechanics and Materials, Vols. . pp. 4589-4597. ISSN ISSN: 1662-7482

Full text available as:
[img] PDF - Published Version
Restricted to Registered users only

Download (796Kb) | Request a copy

    Abstract

    Unsteady Reynolds-Averaged Navier-Stokes computations are presented for the flow over a pure plunging aerofoil and a plunging wing. The implicit RANS solver used for obtaining time-accurate solution is based on implicit finite volume nodal point spatial discretization scheme with dual time stepping. Baldwin and Lomax turbulence model has been used for the turbulence closure. The results are obtained in the form of aerodynamic coefficients, thrust coefficient and propulsion efficiency for two different cases over the aerofoil and wing and are compared with available literature.

    Item Type: Journal Article
    Subjects: AERONAUTICS > Aeronautics (General)
    AERONAUTICS > Aerodynamics
    Division/Department: Computational and Theoretical Fluid Dynamics Division , Computational and Theoretical Fluid Dynamics Division
    Depositing User: Mr Siva kumar Kolkondi
    Date Deposited: 02 Jul 2012 10:30
    Last Modified: 02 Jul 2012 10:30
    URI: http://nal-ir.nal.res.in/id/eprint/10492

    Actions (login required)

    View Item