- #1
lnpsivan
- 5
- 1
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 putting the entire claculation process into an iterative loop...hence...any advice on possible references or similar programs would greatly help...
one other issue is that...in matlab...if i say
for x=1:1:3
y=2*x
end
how should i alter t above command to make all the values of y thru this loop get stored in a "y" matrix. i.e. wat command shud i put to get a result like this
y=2 4 6
any constructive advice is much appriciated...
thanx
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 putting the entire claculation process into an iterative loop...hence...any advice on possible references or similar programs would greatly help...
one other issue is that...in matlab...if i say
for x=1:1:3
y=2*x
end
how should i alter t above command to make all the values of y thru this loop get stored in a "y" matrix. i.e. wat command shud i put to get a result like this
y=2 4 6
any constructive advice is much appriciated...
thanx