posted 12-30- 07:12 AM
If you are interested in editing the airfoils for your OpenPlane project, this is the best web page I found in terms of gaining the needed knowledge to edit the airfoil data:
http://beadec1.ea.bs.dlr.de/Airfoils/veldistr.htm Here you will find the definition of Lift Coefficient, Drag Coefficient, and Moment Coefficient.
Lift Coefficient:
Drag Coefficient:
Moment Coefficient:
Moment refers to the tourque force trying to push the AOA up or down.
If I remember correctly,
L = Lift Force
D = Drag Force
M = Moment Force
p = air density
V = velocity
S = wing area
l = lift force (I think - seems logical)
Here is a screen shot of Etienne's airfoil editor (wing extrator):
The X axis is AOA, -180 on the left, 0 in the center, and +180 degrees on the right
The Y axis is the coef. value.
The red line is the lift coef, the green line is the drag coef, and the blue line is the moment coef. I am not sure what the other 3 lines mean - nether did tailslide it seems - any idia anyone? These other lines are refered to as:
dCl = ?
dCd = ?
dCm = ?
Oh well...
It sure would be nice to have an AOA readout in SDOE
- well was that on the force vector/poly debug screen? I need to try that again and see...
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-Sv =FC=
WWI in SDOE!