sjh7132, the wing is considered stalled when the flow no long remains "attached" to the airfoil surface and lift is reduced. This detachment or separation results in turbulent, lower speed flow near the wing surface. Knowing Bernoulli's principle, as the flow speed is decreased, pressure increases. In the case of an airfoil, this translates to an increase in pressure on the top surface of the wing, effectively reducing the overall lift generated.
what program did you use?
TheSchmidi093 2 months ago
I know what the boundary layer is and how to remove it
WindWisperer99 3 months ago
Do you use Ansys?
Belegetme 5 months ago
Needs more 'draft', punk ;)
1254261 5 months ago
I wonder why 0-shaped wing has stall angle as big as 55°, where the convenient wings stalls at 15-24°?
SEThatered 6 months ago
....COOL
LOZPEACEOUT 11 months ago
This airfoil is generic, based on a NACA profile. Regarding Photoshop...I'm positive it takes less time to simulate this in CFdesign ;)
slimjim8201 1 year ago
Isn't It just Photoshop? ;-)
doppeldeluxe 1 year ago
could somebody please help me out and tell me what exact airfoil is? NACA ...? or what is it? thank you very much! I really appreciate it!
KimiThePilot 1 year ago
@KimiThePilot
Airfoil : surface (as in a wing, propeller, etc.) designed to aid in lifting and controlling an aircraft by means of air currents (Aeronautics)
DaRkAgHoRa 1 year ago
I love it... thanks for upload it. 8)
curva130r 1 year ago
please help me with a tutorial for this animation
toranoko2003 1 year ago
i hear the guy who made this died in a plane crash the VERY NEXT DAY!
161803 1 year ago
Is this supposed to represent a live demonstration, or are those patterns anticipated for each of those particular angles?
sobeita 1 year ago
For this particular wing profile, stalling begins at an angle of attack between 13 and 14 degrees.
slimjim8201 1 year ago
This has been flagged as spam show
@slimjim8201 please can you help me with an tutorial for this animation?
toranoko2003 1 year ago
@slimjim8201 yea thats typical for small cessnas too
srt10taylor 1 year ago
sjh7132, the wing is considered stalled when the flow no long remains "attached" to the airfoil surface and lift is reduced. This detachment or separation results in turbulent, lower speed flow near the wing surface. Knowing Bernoulli's principle, as the flow speed is decreased, pressure increases. In the case of an airfoil, this translates to an increase in pressure on the top surface of the wing, effectively reducing the overall lift generated.
slimjim8201 1 year ago 3
@slimjim8201 Max lift occures after stall.
chujciwdupedwarazy 1 year ago
At what point is the wing officially considered stalled? When the flow starts to separate from the top? When it's completely separated?
sjh7132 1 year ago
finite element analysis
CallmeCrash1969 2 years ago
Yes, CFdesign uses an FEA approach to CFD.
slimjim8201 3 years ago
is this finite element method?
Adrianrff 3 years ago