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Aerodynamic Calculation of Multi-element High-lift Airfoil with a Pressure-based Algorithm and NVD Technique

In: Current Trends in High Performance Computing and Its Applications

Author

Listed:
  • M. H. Djavareshkian

    (University of Tabriz, Faculty of Mechanical Engineering)

  • S. Memarpour

    (University of Tabriz, Faculty of Mechanical Engineering)

Abstract

An improved pressure-based procedure to solving Navier Stokes equations on a nonorthogonal mesh with collocated finite volume formulation is developed for incompressible flows. The boundedness criteria for this procedure are determined from NVD scheme. The procedure incorporates the K — ε eddy-viscosity turbulence model. The aim of the present study is to develop above scheme in incompressible flow and investigate the calculation of this flow around the multi-element airfoils. The results of this simulation around the multi-element airfoil MDA 30P-30N are compared with numerical data. Computation visualization of the external flows show that the algorithm presented in this paper is successful in incompressible regime for coarse meshes.

Suggested Citation

  • M. H. Djavareshkian & S. Memarpour, 2005. "Aerodynamic Calculation of Multi-element High-lift Airfoil with a Pressure-based Algorithm and NVD Technique," Springer Books, in: Wu Zhang & Weiqin Tong & Zhangxin Chen & Roland Glowinski (ed.), Current Trends in High Performance Computing and Its Applications, pages 277-282, Springer.
    • Handle: RePEc:spr:sprchp:978-3-540-27912-9_31
    DOI: 10.1007/3-540-27912-1_31
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