Questions about ReTheta & Gamma setup in airfoil calculation

kevin.pku · December 4, 2018, 21:53

Dear all,

I am calculating the NACA 64312 airfoil. The freestream velocity is 50m/s, the turbulent intensity is 1%. I use the Komega SSTLM transition model for calculation and my setup for U, k and Rethetat are shown in the attached figures. Unfortunately, the calculation fails. There may be some errors in
my setup. Could anyone help me? Thank you.

u.JPG

k.JPG

ReThetat.JPG

akamal1099 · May 6, 2022, 15:13

Hello Sir,
Did you solve the issue, I am experiencing similar issue today.
Thanks

Dipanshu Pant · January 4, 2023, 06:04

Quote:

Originally Posted by kevin.pku

Dear all,

I am calculating the NACA 64312 airfoil. The freestream velocity is 50m/s, the turbulent intensity is 1%. I use the Komega SSTLM transition model for calculation and my setup for U, k and Rethetat are shown in the attached figures. Unfortunately, the calculation fails. There may be some errors in
my setup. Could anyone help me? Thank you.

Attachment 67112

Attachment 67113

Attachment 67114

Try correcting the fvSchemes and fvSolution, there is a case in wolf dynamics tutorial where he has done naca0012_transonic, I used those schemes and solution and it worked for me. Best of luck

December 4, 2018, 21:53	Questions about ReTheta & Gamma setup in airfoil calculation	#1
kevin.pku New Member kevin Join Date: Oct 2018 Posts: 6 Rep Power: 7	Dear all, I am calculating the NACA 64312 airfoil. The freestream velocity is 50m/s, the turbulent intensity is 1%. I use the Komega SSTLM transition model for calculation and my setup for U, k and Rethetat are shown in the attached figures. Unfortunately, the calculation fails. There may be some errors in my setup. Could anyone help me? Thank you. u.JPG k.JPG ReThetat.JPG

May 6, 2022, 15:13	Inquiry	#2
akamal1099 New Member Abdelrahman Kamaleldin Join Date: Jan 2021 Posts: 6 Rep Power: 5	Hello Sir, Did you solve the issue, I am experiencing similar issue today. Thanks

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