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"The vertical stabilizers, vertical stabilisers, or fins, of aircraft, missiles or bombs are typically found on the aft end of the fuselage or body, and are intended to reduce aerodynamic side slip and provide direction stability. It is analogous to a skeg on boats and ships. On aircraft, vertical stabilizers generally point upwards. These are also known as the vertical tail, and are part of an aircraft's empennage. The trailing end of the stabilizer is typically movable, and called the rudder; this allows the aircraft pilot to control yaw... A V-tail has no distinct vertical or horizontal stabilizers. Rather, they are merged into control surfaces known as ruddervators which control both pitch and yaw. The arrangement looks like the letter V, and is also known as a butterfly tail. The Beechcraft Bonanza Model 35 uses this configuration, as does the F-117 Nighthawk, and many of Richard Schreder's HP series of homebuilt gliders." The fin does not have to be at 90 degrees to provide stability and pitch control.I am sure an off-set fin would not cause noticeable control problems in a model, provided it is still vertical enough to act as a stabilizer, and the rudder moves freely.I am not advocating our putting planes together in a slap-dash way, but suggesting it is possible to worry too much about perfection. |
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The main effect for flying with a tilted vertical stabilizer is that there will be some pitch coupling with rudder input. At the extreme, with the vertical stab tilted 90 degrees, it would then be a horizontal stab and the rudder would become the elevator. The pitch coupling from one or two degrees of tilt would not even be noticeable in most RC planes. And since most RC flyers seldom, if ever, use the rudder while flying it really would have no effect at all.
Larry |
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Withe the vertical stab 5-10 deg. off vertical from the horizontal stab, the plane will have a wider turning circle to one side (and keep the altitude a tad better while turning) and a narrower turning circle loosing altitude a bit faster in the other direction - the effects of the pitch coupling mentioned by Lnagel... How I know? From countless hours of flying Champs in various states of repair
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Joined Nov 2008
414 Posts
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Edmond |
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