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کلمات کلیدی: NACA 0012 airfoil
موارد یافت شده: 4
1 - Rarefied gas flow simulations of NACA 0012 airfoil and sharp 25–55-deg biconic subject to high order nonequilibrium boundary conditions in CFD (چکیده)2 - Investigation of aerodynamic characteristics of rarefied flow around NACA 0012 airfoil using DSMC and NS solvers (چکیده)
3 - INVESTIGATION OF RAREFIED GAS FLOW AROUND NACA 0012 AIRFOIL USING DSMC AND NS SOLVERS (چکیده)
4 - Investigating the effects of numerical discretisation on the accuracy of incompressible turbulent flow solution around NACA 0012 airfoil (چکیده)
