Different Drag coefficient value???
Thats my graduated project and i got different values every time to calculate the drag coefficient. On ansys i have a mesh naca0012 airfoil 2d profile which has 247000 nodes and start the analysis on fluent. I work transient flow and these are my parameters to take
This is meshhttps://www.cfd-online.com/Forums/at...1&d=1543594720 Mesh information https://i.hizliresim.com/7aVLzl.png In fluent this is my reference values and time, type https://i.hizliresim.com/gr4GaN.png Turbulance Models https://i.hizliresim.com/qdmDoq.png Solution Method(i solve second order) https://i.hizliresim.com/P1YV98.png This is my calculation page https://i.hizliresim.com/LlY6rV.png and the result(Mine) https://i.hizliresim.com/r5mDrP.png Result(which i based on)https://i.hizliresim.com/9a97J8.png in this image Cdw is the drag coefficient* Our drag coefficient is different then thesis and i have to figure out this problem. Also lift coefficient is different too but not so much as drag coefficient. What is my wrong(s)? thanks for helping btw. |
All your pics disappeared
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As a guess, you have not set the reference values in accordance to your problem.
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