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]

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