Обтекание крыловых профилей NACA0012 и NACA0021

Документы, презентации и анимации
pdf 2001_Swalwell, Sheridan, Melbourne_The effect of turbulence intensity on stall of the NACA 0021 aerofoil
Экспериментальная статья по обтеканию NACA0021

pdf 2003_Swalwell, Sheridan, Melbourne_Frequency analysis of surface pressures on an airfoil after stall
Экспериментальная статья по обтеканию NACA0021

pdf 2005_Swalwell_The effect of turbulence on stall of horizontal axis wind turbines
Экспериментальная статья по обтеканию NACA0021

pdf 2009_Garbaruk et al._Evaluation of Time Sample and Span Size Effects in DES of Nominally 2D Airfoils beyond Stall
Garbaruk, A., Leicher, S., Mockett, C., Spalart, P., Shur M.L., Strelets, M.Kh., Thiele, F. Evaluation of time sample and span size effects in DES of nominally 2D airfoils beyond stall. Proceedings of Third Symposium on Hybrid RANS-LES Methods, 10-12 June 2009, Gdansk, Poland (19 pages).

pdf 2009_Garbaruk et al._NACA0021 at 60
Garbaruk, A., Shur, M., Strelets, M., Travin, A. NACA0021 at 60 deg. incidence. In: Haase W, Braza M, Revell A (eds) “DESider – A European Effort on Hybrid RANS-LES Modelling”. Notes on Numerical Fluid Mechanics and Multidisciplinary Design, Vol. 103. Springer, 2009, pp. 127-139.

pdf Pres_NACA
Презентация о проведении RANS и DDES расчетов обтекания крыловых профилей NACA0012 и NACA0021