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June 3, 2001, 02:36 |
Looking for 2-D unsteady panel method code
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#1 |
Guest
Posts: n/a
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I am looking for 2-D unsteady panel method code.Who can tell me where I will find it? Any help would be appreciate.
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June 21, 2001, 00:44 |
Re: Looking for 2-D unsteady panel method code
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#2 |
Guest
Posts: n/a
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I have written a panel method program, would you like me to find it and send it to you?
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April 27, 2009, 01:35 |
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#3 |
New Member
Ashok
Join Date: Apr 2009
Posts: 1
Rep Power: 0 |
Can anyone send me the 2-D unsteady panel method code written either in matlab or fortran. it would be of great help if you can provide me this.
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May 2, 2009, 05:22 |
need to dedug my unsteady panel code ,else need unsteady panel code
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#4 |
New Member
T.Rajesh Senthil Kumar
Join Date: May 2009
Location: India, Tamil Nadu, Coimbatore
Posts: 3
Rep Power: 16 |
am doing my Mtech Project on Flapping foil aerodynamics.. am written unsteady vortex panel code in matlab.. but its not converging after three time steps.. if any one wish to debug my code.. i will send the code.. i need help in debugging my code... if anyone have code in fortan or Matlab,kindly send it to me.. it will be helpful to rectify my errors..
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May 5, 2009, 13:08 |
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#5 |
Senior Member
N/A
Join Date: Mar 2009
Posts: 189
Rep Power: 17 |
XFoil would work
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January 20, 2011, 12:49 |
2D unsteady panel method kutta condition
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#6 |
New Member
Amit Singh
Join Date: Jan 2011
Posts: 3
Rep Power: 15 |
Hi,
I'm working on a 2D unsteady panel method for harmonic oscillations of a NACA 0012 airfoil. I've been trying to debug the code for ages. I'm getting a nice sinosoidal variation for the lift force but the value of amplitudes are not satisfactory. Does anyone have any source to verify the values I'm getting. Also, while implementing the kutta condition(Basu and Hancock), I'm getting a quadratic equation. So, to choose the correct root, the one closest to the last time step values is chosen. But at even slightly higher frequencies, the two roots are very close and the code doesn't converge anymore. So, I want to know whether there is a better way to choose the correct root so that I can reach higher frequencies. Thank You. |
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