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For questions on an airplane's main wing
9
votes
Accepted
Are aircraft with squirrel cage fans as wings viable?
The paper utilizes the projected area of the cycloidal rotor (the "drum", if you will, the forms the fan wing concept). … I've seen more CAD of fan-wing designs than I have vehicles (at least, for those larger than the MAV scale), so I'm inclined that think it's not living up to expectations for the larger vehicles, but that's …
14
votes
Accepted
Could an airplane dock with a set of wing extensions while airborne?
Also, more reading can be found in this text Flying Aircraft Carriers of the USAF: Wing Tip Coupling by Brian Lockett.
Naturally, there were significant downsides to this idea. … Due to conflicting requirements on wing structure and aircraft weight, I think that ultimately didn't fly...but I don't have any of the details for that. …
16
votes
Accepted
What is the function of the leading edge strip?
A picture of this from a wing I built is below (the leading edge is on the left hand side -- and just ignore the fact that the wing is twisted...). … However, the addition of a structural element, such as a leading edge cap, that goes the length of the wing adds a non-negligible amount of torsional stiffness to the wing. …
3
votes
Would a wingtip stall still be bad if there was no aileron there?
The left wing is stalled (operating at an even higher angle of attack than the right wing): it's lift coefficient is much lower than that of the right wing: the airplane wants to roll. … If the lift production of the stalled wing remains less than that of the other wing, the aircraft will continue to roll. …
8
votes
Can this design provide more lift force than thrust from engine?
(Propeller/wing interaction) in the 1980s recorded a wing seeing up to 40% savings in induced drag based on the adjustment of a tractor propeller's rotation rate! … If you have a small enough wing, though, say on the scale of UAV, there's a good chance you could have a significant portion of your wing in the propwash, which can keep the flow attached to the wing at …