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. In: 2011 International Conference on Mechanical and Aerospace Engineering (CMAE 2011), March 21-23, 2011, SRM University, Modi Nagar Campus,Delhi-Meerut Road, Sikrikalan Modi Nagar, Gazhiabad, Uttar Pradesh - 201 204.

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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: Conference or Workshop Item (Paper)
Subjects: AERONAUTICS > Aerodynamics
Depositing User: Mr Siva kumar Kolkondi
Date Deposited: 30 Mar 2011 04:49
Last Modified: 24 Sep 2015 05:28
URI: http://192.168.9.127/id/eprint/9169

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