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AOA Port in LEADING EDGE - Where to locate (or won't work)
I know this must have been figured out. I plan on using EFIS AOA (Dynon,
Garmin, GRT) but not a fan of the Pitot/AOA port in one. These AOA's work (with out a vane) is comparing pressure of pitot vs the AOA port. The difference in pressure between the two gives you derived AOA. Right? (correct me if wrong). Want to use a small pitot (only) under wing, and place the AOA port in the leading edge. WHERE DO I LOCATED THAT AOA PORT in LEADING EDGE? Would this not work? Suppose Dynon/Garmin/GRT software might not be ideal for this configuration. The other way to go is stall warning vane or tab... Van has one in his catalog. |
This thread has the info you need: http://www.vansairforce.com/communit...ad.php?t=34040
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I'm not going to read that old thread, but for my AFS Sport AoA, the manual reads:
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Quote:
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email sent.
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I used a pop-rivet with the mandrel punched out (similar to static port) near my leading edge landing light cutout. I can access the tube/rivet junction inside the cutout.I tried to match the angle of the Dynon/Garmin pitot tubes for the AOA port vs the leading edge.
It does work but is too sensitive, it seems to bounce around a lot especially in turbulence and turns. I?ve been thinking about adding a probe/straw and get out of the boundary layer. |
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