Algorithm of mesh adaptation for accurate aerodynamic simulation in cfd code FlowVision

Authors

  • P. I. Karasev Moscow Aviation Institute (National Research University) (Moscow, Russian Federation)
  • A. S. Shishaeva Moscow Institute of Phisics and Technology (State University) (Moscow, Russian Federation)
  • A. A. Aksenov Moscow Institute of Phisics and Technology (State University) (Moscow, Russian Federation)

DOI:

https://doi.org/10.14529/cmse120205

Keywords:

computational fluid dynamics, computational grid, adaptation to solution, airfoil, aerodynamic characteristics

Abstract

Influence of mesh adaptation on getting accurate aerodynamic characteristics of airflow over wing profiles in CFD code FlowVision is investigated. Algorithm of adaptation criteria for accurate and fast solving aerodynamic problems is created on basis of this investigation. Conclusions done in this paper is possible to apply for solving different aerodynamic tasks more complex then airfoils.

References

Aksenov, A.A. Overcoming of Barrier between CAD and CFD by Modified Finite Volume Method / A.A. Aksenov, A.A. Dyadkin, V.I. Pokhilko // Proc. of “1998 ASME Pressure Vessels and Piping Division Conference” (San Diego, ASME PVP). – 1998. –Vol. 377-1.

Gregory, N. NPL 9615 and NACA 0012. A Comparison of Aerodynamic Data / N. Gregory, P.G. Wilby. Ministry of Defense, Aeronautical Research Council. – London: Her Majesty’s Stationery office. – C.P. No. 1261, 1973. – 56 p.

Кашафутдинов, С.Т. Атлас аэродинамических характеристик крыловых профилей / С.Т. Кашафутдинов, В.Н. Лушин. – Сибирский НИИ Авиации им. С.А. Чаплыгина, 1994. – 74 c.

Published

2012-01-14

Issue

Section

Numerical Mathematics