off the top of my head...i am not sure so don want to advice..but in case somethin does come up..shall pass on t info...sorry wasnt of any direct help...
thanx for the offer...
about your question..i need to think...if i can recall there are/were only a very few swept wing bi-planes
y would u need it? if i may ask...
vortex panel method can't cater for sweep, unless you are trying calculate the normal component of the flow as the wing "sees"...
yes i realized that...nevertheless thanks for the advice..much appriciated...
from the time i posted the first entry in this thread i hav gone on to write 5 aerodynamic analysis programs in MATLAB...
-flat plate solution for "n" lumped vortex at an angle "alpha" to flow;
-numeric lifting line...
hi,
i am in the final yr aerospace engg...i am trying to write a program on MATLAB to calculate the lift distribution over a wing using the numerical estimation based on the classic(prandtl) lifting line theory...however, due to my relatively limited exposure to MATLAB i am having trouble...