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![]() Allen wrote: wrote in message oups.com... Allen wrote: wrote in message ups.com... Allen wrote: I once saw a pair of mechanics doing a full power run-up in a Maule. They were holding brakes on and forward elevator, the tail was about six feet in the air standing still. So yes. Why do you separate the nosewheel from the tailwheel? They both fly with the same principles. Allen Aha, but you have to allow for the thrust line being so far above the drag line, which in this case is the ground where the wheels are locked. That thrust produces a pitching couple that raises the tail much more effectively than the down-elevator. If the pilot holds full forward elevator at the start of the takeoff roll, the tails of most taildraggers won't come up until some considerable forward speed is attained, and then the tail is rising mostly because the centre of pressure of the wing, being behind the mains, is lifting it. Using forward elevator will lift the tail sooner but it sure is not entirely responsible for the rise. Wheelbarrowing is also mostly caused by too-fast landing speeds, not just forward elevator. It's worse with flaps down because the wing's CP is ahead of the mains and is raising the tail. Down-elevator isn't even necessary at high-enough speeds. The nosewheels of most trikes is closer to the ground than the mains in level flight attitude, and will contact first with the high airspeed reducing AOA. Dan (Instructor in taildraggers and trikes and a mechanic too) I have seen a Super Cub land with a 40 knot (or so) headwind and come to a complete stop, then raise the tail off the ground with the engine at idle. I see you point about the thrust affecting pitch though, used that all the time landing the Lear, as you bring the power levers to idle the nose pitches up and automatically puts you into the flare. Allen But that 40-knot headwind is still lifting the wing, even with the airplane motionless, making it very easy for the elevator to LIFT THE TAIL. The airplane is almost flying. Dan Ah ha, the answer to the OP's question. Allen Sort of. But when flying a taildragger, you soon learn that the elevator's tail-raising ability isn't very strong at all. When we teach normal takeoffs in the Citabria, we accelerate with the elevator neutral (wherever it wants to be) until the tail rises about four inches off the pavement, then begin applying back pressure to keep it from coming up any more. By the time it flies off, you have considerable up-elevator in just to keep the tail down in climb attitude, and that force will be required, with reduction as speed increases, until climb speed is reached and stabilized. At that time the stabilizer's downforce will be strong enough to keep the airplane in climb attitude. If we applied no backpressure during takeoff, the tail would rise alarmingly to level flight attitude all on its own. If solo, the nose could get pretty low. The wing is lifting, and since the airplane is designed to go nose-down when speed is low, it will do just that as the wings take the weight off the wheels. When we do tail-high takeoffs, we apply full forward stick to get the tail up much sooner, but as speed builds backpressure will be needed at some point to control the attitude. Can't blame all the attitude changes on the elevator. The wing's lift as opposed to the wheels placement also has a huge effect. We have balanced airplane models we use to demonstrate these things to the students. They can see the tail come up when we lift the wing at CP with our fingers and wheels leave the table. Dan |
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