Numerical Study on Low Reynolds Number Flows Over an Aerofoil
نویسندگان
چکیده
منابع مشابه
Numerical Simulation of Unsteady Low-Reynolds-Number Separated Flows over Airfoils
boundary-layeredge is still slightly freestreamdependent, the level of eddy viscosity and therefore also the skin-friction coef cient are not. Furthermore, the velocity distribution is consistent with the law-of-the-wall solution. As a second test case, the RAE2822 airfoil is considered (in particular, case 9 of Ref. 11). Figure 2 compares the pressure and skinfriction distributions of the dif...
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ژورنال
عنوان ژورنال: Journal of Applied Mechanical Engineering
سال: 2013
ISSN: 2168-9873
DOI: 10.4172/2168-9873.1000131