Lam Aileron Design
Lam Aileron Design
(OP)
Fascinating new aileron/flap/spoiler integrated design concept. I see significant potential with the design concept for new designs that can integrate "the system" from the start! http://lamaviation.com/ [click-on the video http://www.youtube.com/watch?v=RXedpHTQYJ0 for a straightforward understanding of the concept].
Note: My dad built a Thorp T-18 when I was a Kid. John Thorp solved the adverse-drag problem by having differential ailerons: 2X-Up, 1X-down... using clever bellcrank geometry.
Note: My dad built a Thorp T-18 when I was a Kid. John Thorp solved the adverse-drag problem by having differential ailerons: 2X-Up, 1X-down... using clever bellcrank geometry.
Regards, Wil Taylor
RE: Lam Aileron Design
B.E.
RE: Lam Aileron Design
TTFN
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RE: Lam Aileron Design
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RE: Lam Aileron Design
Kenat... I suspect the structural penalty would be significant... especially torque and rear-spar point loads. You think narrow chord surfaces could mitigate this a bit... and still have aero advantages?
Regards, Wil Taylor
RE: Lam Aileron Design
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RE: Lam Aileron Design
But, the Lam sflapoileron is quite versatile. You could certainly see it finding a home on a flying wing UAV.
RE: Lam Aileron Design
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RE: Lam Aileron Design
http://www.sailplanedirectory.com/schempp.htm
Wil, I am having a little difficulty getting a good picture of this.
Scroll down the directory to the Nimbus 3 and read the following description of the aileron operation,"" When rolling at large aileron deflection, the spoiler flap deploys to compensate for lack of rudder to permit coordinated flight"". There is a picture in the upper right hand showing the aircraft in a steep turn to the right with the tip spoileron partially deployed.
The later Nimbus 4 uses the same system.
Brian E.
RE: Lam Aileron Design