Author:
Pasha Khaled M.K.,Elfawal M.M.
Reference16 articles.
1. airfoil tools, NACA6409 9% (n6409-il) Xfoil prediction polar at RE=1,000,000 Ncrit=9, updated 2020. http://airfoiltools.com/polar/details?polar=xf-n6409-il-1000000.
2. Investigation on the correlation of Cfd and EFD results for a supercritical wing;Liu;Int. J. Heat Technol.,2015
3. Numerical simulation research on the transonic aero-elasticity of Aa high-aspect-ratio wing;Hongtao;Int. J. Heat Technol.,2015
4. Judith Geyr, Fedime Knoblauch z. von Hatzbach, Arne Seitz, Thomas Streit, Georg Wichmann, Wing Design Based on a Tapered Wing Natural Laminar Flow Airfoil Catalogue, New Results in Numerical and Experimental Fluid Mechanics IX (2014), pp 183-191|January.
5. Application of multibody simulation tool for dynamical analysis of tethered aerostat;Mahmood;J. King Saud Univ. – Eng. Sci.,2020
Cited by
1 articles.
订阅此论文施引文献
订阅此论文施引文献，注册后可以免费订阅5篇论文的施引文献，订阅后可以查看论文全部施引文献