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February 12, 2015, 02:59 |
2d flutter calculation
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#1 |
Member
varghese mathew
Join Date: Aug 2014
Location: India
Posts: 32
Rep Power: 11 |
i am using 2d flutter code using the typical wing section model provided in the su2_cfd in-buit code .i am having problem to compute flutter boundary of a given airfoil. for the given mach no i am getting only one response at a particular mach no i want to plot the three responses (damping , neutral and diverging ) at a particular fixed mach no.can any body help me stating what is the parameter to be changed in the config file to obtain the diffrent response at a particular fixed mach no .
Last edited by varghese9; March 6, 2015 at 13:13. |
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