Computations of Flow Over the Hump Model Using Higher-Order Method With Turbulence ModelingThe flow over the two-dimensional hump model is computed by solving the RANS equations with kappa-omega (SST) model. The governing equations, the flow equations and the turbulent equations, are solved using the 5th order accurate weighted essentially non-oscillatory (WENO) scheme for space discretization and using explicit third order total-variation-diminishing (TVD) Runge-Kutta scheme for time integration. The WENO and the TVD methods and the formulas are explained in [1] and the application of ENO method to N-S equations is given in [2]. The solution method implemented in this computation is described in detail in [3].
Document ID
20070031073
Acquisition Source
Langley Research Center
Document Type
Conference Paper
Authors
Balakumar, P. (NASA Langley Research Center Hampton, VA, United States)
Date Acquired
August 24, 2013
Publication Date
April 1, 2007
Publication Information
Publication: Proceedings of the 2004 Workshop on CFD Validation of Synthetic Jets and Turbulent Separation Control
IDRelationTitle20070031059Collected WorksProceedings of the 2004 Workshop on CFD Validation of Synthetic Jets and Turbulent Separation Control20070031059Collected WorksProceedings of the 2004 Workshop on CFD Validation of Synthetic Jets and Turbulent Separation Control