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Speed control is OPPOSITE to that during aerotow and gliding
I'm sure if I asked this of one of our instructors the answer would be "you don't" You control the attitude, the winch driver controls the speed. Lowering the nose is the signal to the driver that you are too slow, wagging the rudder the signal for too fast. If the winch driver doesn't or cannot respond you abandon the launch. Roger Worden wrote: What is the correct relationship between pitch angle and airspeed during ground launch, either by auto or winch? Different sources make conflicting statements: 1. Speed control is OPPOSITE to that during aerotow and gliding * SSA Soaring Flight Manual, page 13-10: "Under most circumstances, the best way to reduce the airspeed is to raise the nose. During ground launch, however, the opposite is true ... pulling the nose up results in an increase in airspeed, assuming the launch vehicle has adequate power." * FAA Glider Flying Handbook, page 7-16: "The pitch attitude/airspeed relationship during ground launch is unique. During the launch, pulling back on the stick tends to increase airspeed, and pushing forward tends to reduce airspeed. This is the opposite of the normal pitch/airspeed relationship." * This is what I was taught during autotow training. I can't say that I have varied the pitch enough in my few launches to have demonstrated it. 2. Speed control is the SAME as during aerotow and gliding * British Gliding Association Instructors' Manual, page 16-2: "If the launch speed starts to tail-off, lower the nose." Page 16-3: "monitor the airspeed trend. If it is falling back towards the minimum safe speed, lower the nose or relax any back pressure on the stick." BGA does not mention attempting to slow down: "If the glider is starting to go too fast, maintain the normal climb attitude, and signal. If it remains too fast, or gets even faster, release." * During presentations on winch launch at a recent seminar, two leading instructors discussed lowering the nose to increase speed and raising the nose to decrease speed. * This is what my experience with the Condor flight simulator winch launch has shown. It seems to me that this is a critical point on which to be clear, since I will be winch-launching for the first time soon. I understand that the vectors involved are different than in aerotowing, because the wings are converting forward rope travel to angular motion (just like the skeg on a water ski!). I also understand that a properly balanced glider using a CG hook for winch launch will tend to nose up initially, and will seek an optimal climb angle naturally. Altering the climb angle with elevator will necessarily result in a less-than-optimal altitude gain. But what is the actual effect of raising or lowering the nose in a stable ground launch climb? A. Is it different depending on the angle of climb? In my experience, autotows tend to achieve a 25- to 30-degree climb angle, winch launch a 40- to 45-degree climb. Does that cause a difference in the effect of pitch angle? B. If #2 above is true, how did the SSA and FFA manuals get it wrong? C. If #1 is true, is it reversed in Britain? (Just kidding...) |
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![]() "ucsdcpc" wrote in message ... Speed control is OPPOSITE to that during aerotow and gliding I'm sure if I asked this of one of our instructors the answer would be "you don't" You control the attitude, the winch driver controls the speed. Lowering the nose is the signal to the driver that you are too slow, wagging the rudder the signal for too fast. If the winch driver doesn't or cannot respond you abandon the launch. And your instructor would be wrong in most cases. Pilots who think they are controlling attitude are at risk of stalling while on the cable. We are in a transition period in winch launch where old ideas are giving way to the new. New gliders launched by new winches operate by somewhat different rules. In the modern view, the winch driver controls POWER and the pilot controls AIRSPEED. The relationship is the same as in airplanes where throttle controls power and pitch controls airspeed. As the glider leaves the ground on a winch launch. the pilot smoothly pitches up to hit a target climb airspeed. In an airplane, this would be Vy. In the typical glider, it will be between 55 and 65 knots depending somewhat on headwind. It's helpful to think of the winch driver as your flight engineer with his hands on the power levers. A modern trainer such as a ASK-21 would need a very powerful winch indeed for its pilot to be unable to control airspeed. In most cases, the entire launch will be flown with neutral elevator leaving considerable up elevator to control airspeed. An important exception is with gliders which have hooks too far forward and/or have too little up elevator authority - for example, most Schweizers. When flying these gliders the pilot will reach full up elevator before the airspeed can be controlled. Since the pilot cannot control airspeed, the winch driver has to. A further complication is that these gliders, which require the winch driver to control airspeed, will not reach more than 1/2 to 2/3's the height of the modern 2-seater with a properly positioned CG hook. This exception case also introduces complications in the event of a cable break. With the elevator positioned at full up, the glider will pitch up strongly at the cable break - sometimes beyond the point where a safe recovery can be made. In any event, a very quick and positive action will be required of the pilot. This contrasts with gliders like the ASK-21 which will continue on the same trajectory giving the pilot additional seconds to handle the cable break. Bill Daniels |
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