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On Sat, 09 May 2009 12:35:38 -0500, Jim Logajan
wrote: "RST Engineering - JIm" wrote: Those might get me airspeed but I'm not at all sure how you would get theta from any one of these schemes. I believe he means the vane is lightweight and freely pivots up or down so that it is always pointing into the relative wind. The angle the vane makes with some reference line on the wing or fuselage is thus the AoA. I'd post a link to a picture of what it would look like (pretty simple concept) but can't see to find one! Just think of the yaw string on gliders (e.g. the red string in this pictu http://www.highonadventure.com/Hoa08...eYawString.jpg) but used to show vertical component of the relative wind, not horizontal. Use variable capacitance, variable reluctance, resistor strip or synchro connected to a vane. For a real giggle do as some Air Force systems and employ a slotted, rotating cone for a probe. It involves a feedback loop. Dan, U.S. Air Force, retired See http://www.pegazair.on-the-net.ca/Cl...rframe/lri.htm and use electronic differential pressure in place of the DWYER MINIHELIC II. The diagram of the probe dissapeared, sorry. |
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