skatj
Nov 07, 2007, 12:11 AM
I'm trying to figure out the amount of wing area I need to lift off for a 2 lb airplane.
Using the formula L = 1/2 d v^2 s Cl
I rewrote the equation as 2L/ d v^2 Cl = s
I plugged in 2 as the lift needed, 0.002377 as the density of the air, 25 as velocity squared, and 1 as the coefficient of lift (I read somewhere that this was an acceptable number for most model aircraft).
Anyway turns out I needed 67 square feet of wing area to take off. So umm...
I'm retracing my steps to see where I went wrong when some questions came up.
1) Is the amount of lift needed to take have equal to the weight of the aircraft or the wing loading of the aircraft? Because the wing loading would be significantly lower.
2) Does the lift need to be equal to the downward force, or does it actually have to be somewhat greater than it?
3) How do I take into account the angle of the elevator when calculating lift?
4) Is 5 ft/s a good ballpark estimation for a 2 lb plane with a brushed motor on the ground that's taking off?
5) Should I be using 1 as the lift coefficient?
On a sidenote, what is a light wing loading for the slowest, most stable flight possible? Maybe I'll just try to get a wing area estimation from that.
Using the formula L = 1/2 d v^2 s Cl
I rewrote the equation as 2L/ d v^2 Cl = s
I plugged in 2 as the lift needed, 0.002377 as the density of the air, 25 as velocity squared, and 1 as the coefficient of lift (I read somewhere that this was an acceptable number for most model aircraft).
Anyway turns out I needed 67 square feet of wing area to take off. So umm...
I'm retracing my steps to see where I went wrong when some questions came up.
1) Is the amount of lift needed to take have equal to the weight of the aircraft or the wing loading of the aircraft? Because the wing loading would be significantly lower.
2) Does the lift need to be equal to the downward force, or does it actually have to be somewhat greater than it?
3) How do I take into account the angle of the elevator when calculating lift?
4) Is 5 ft/s a good ballpark estimation for a 2 lb plane with a brushed motor on the ground that's taking off?
5) Should I be using 1 as the lift coefficient?
On a sidenote, what is a light wing loading for the slowest, most stable flight possible? Maybe I'll just try to get a wing area estimation from that.