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-   -   cl,cd data for pitching/plunging airfoil at low Re (https://www.cfd-online.com/Forums/main/10745-cl-cd-data-pitching-plunging-airfoil-low-re.html)

Quarkz February 3, 2006 22:22
cl,cd data for pitching/plunging airfoil at low Re
 
Does anyone know of reference (numerical/experimental) for cl, cd, cp (lift,drag, pressure coefficient) data for pitching/plunging airfoil at low Re, preferably around 100 - 500?

I need it for comparison against my incompressible NS solver.

Thanks

amir.f August 9, 2011 03:11
Quote:
Originally Posted by Quarkz
;40297
Does anyone know of reference (numerical/experimental) for cl, cd, cp (lift,drag, pressure coefficient) data for pitching/plunging airfoil at low Re, preferably around 100 - 500?

I need it for comparison against my incompressible NS solver.

Thanks
hi i want too valid my incompressible NS code for pure plunging airfoil. can you find any data for your validation?
Thanks


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