Siva Kumar , K and Sharanappa, Sajjan V (2011) Unsteady Flow past a Combined Pitching and Plunging Aerofoil 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.
|PDF - Published Version |
Unsteady Reynolds-averaged Navier-Stokes (RANS) computations are presented for low Mach number flow past a combined pitching and plunging NACA 0012 aerofoil. The Implicit RANS solver used for obtaining timeaccurate solutions is based on a finite volume nodal point spatial discretization scheme with dual time stepping. The aim is to validate the unsteady solver for flapping motion of the aerofoil. Results are presented in the form of aerodynamic coefficients and compared with available literature, thus demonstrating the capability of the solver to provide useful unsteady input data for aeroelastic and aeroacoustic analysis.
|Item Type:||Conference or Workshop Item (Paper)|
|Subjects:||AERONAUTICS > Aerodynamics|
|Division/Department:||Computational and Theoretical Fluid Dynamics Division , Computational and Theoretical Fluid Dynamics Division|
|Depositing User:||Mr Siva kumar Kolkondi|
|Date Deposited:||30 Mar 2011 10:21|
|Last Modified:||27 Aug 2012 12:14|
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- Unsteady Flow past a Combined Pitching and Plunging Aerofoil using an Implicit RANS Solver. (deposited 30 Mar 2011 10:21)[Currently Displayed]
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