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#1 |
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thank you very much! my email address:zhubiao2006@gmail.com
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#2 |
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I also need 3d models of airfoil , can you please help me in thatv
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#3 |
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the mbb-a3 airfoil's equationis: ZL(x)=C(x)-0.5*T(x) ZU(x)=C(x)+0.5*T(x) where: C(x)is camber, T(x) is thickness
C(x)=b1+b2*x+b3*x**2+b4*x**3+b5*x**4 T(x)=a0*sqrt(x)+a1+a2*x+a3*x**2+a4*x**3+a5*x**4 where: b1=0 b2=0.1294408 b3=-0.4206819 b4=0.5516741 b5=-0.2604330 a0=0.2457807 a1=0 a2=-0.2470393 a3=0.5556936 a4=-1.1377743 a5=0.5833393 |
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#5 |
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i m newer to use icem cfd i need help to create an airfoil geometry from x, y data file gratulations
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#6 |
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check cfd tutorial of Cornell University
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