Cp for NACA0012, angle of attack=14degree

October 29, 2008, 05:38

Nowdays, I have calculate a flow for NACA0012 airfoil. The freestream velocity is 30m/s. The angle of attack is 14 degree. In our code, we use a RANS S-A mode with DES. The Cp curve can get from following http://hi.baidu.com/liujmljm/album/i...48cb10dcc.html I am not sure whether the results are right. Who can help me analysis the results? Thank you!

Of couse, if someone has the experimental data or CFD results for this case or other case (angle of attack =15,16,18,... ), and can send to me, i will be very thankful. My email: liujmljm@sina.com

Thank you!!

October 29, 2008, 22:12

Here, Re=1.0e+6

October 29, 2008, 05:38	Cp for NACA0012, angle of attack=14degree	#1
liujmljm Guest Posts: n/a	Nowdays, I have calculate a flow for NACA0012 airfoil. The freestream velocity is 30m/s. The angle of attack is 14 degree. In our code, we use a RANS S-A mode with DES. The Cp curve can get from following http://hi.baidu.com/liujmljm/album/i...48cb10dcc.html I am not sure whether the results are right. Who can help me analysis the results? Thank you! Of couse, if someone has the experimental data or CFD results for this case or other case (angle of attack =15,16,18,... ), and can send to me, i will be very thankful. My email: liujmljm@sina.com Thank you!!

October 29, 2008, 22:12	Re: Cp for NACA0012, angle of attack=14degree	#2
liujmljm Guest Posts: n/a	Here, Re=1.0e+6

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