jcmbl
New member
- Oct 22, 2004
- 31
Guys,
I want to map the pressure distribution from the outer skin onto the camber line. I assume the structural integrity of the airofoil is provided by the camber and no other stiff internal structures. The pressures on both surfaces after mapping are equal if the airfoil is thin (max 6% thickness). What happens if the thickness is larger than 12%? Bernoulli is not that helpfull, but I guess a Laplace domanin technique would do.
Has anyone experienced this sort of issue? What's the best and accurate way to do it?
I appreciate any help.
Regards,
J
I want to map the pressure distribution from the outer skin onto the camber line. I assume the structural integrity of the airofoil is provided by the camber and no other stiff internal structures. The pressures on both surfaces after mapping are equal if the airfoil is thin (max 6% thickness). What happens if the thickness is larger than 12%? Bernoulli is not that helpfull, but I guess a Laplace domanin technique would do.
Has anyone experienced this sort of issue? What's the best and accurate way to do it?
I appreciate any help.
Regards,
J
