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#1
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"Bert Willing" wrote in message ... Ian, winch launching my Calif over 8 years on a 280 hp winch was exactly "full power until release", and that was the only way to go. So, in some cases this type of instructions actually does work. Bert Full power for the whole launch works when the winch is severely underpowered. As more powerful winches are introduced, you will find there are points in the launch where the driver must reduce power to maintain constant tension. Bill Daniels |
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#2
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Should say that it's "full power all the way up" the main climb, of
course we back off at the top. But there was some suprise at the launch point recently when a K21 waved off... the common thought was "K21s should be able to handle it". Maybe it could if it was no wind, but with a good headwind they just can't. So far the sole answer to my original question has been "look at the wingtips during the launch and find what stick position will hold them at about 45 degrees to the horizon AND give a safe speed. If you have a low powered winch you may have to adopt a lesser angle" from Derek. Does everyone agree with this? Dan |
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#3
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Dan G wrote: Should say that it's "full power all the way up" the main climb, of course we back off at the top. But there was some suprise at the launch point recently when a K21 waved off... the common thought was "K21s should be able to handle it". Maybe it could if it was no wind, but with a good headwind they just can't. Headwind makes a big difference. Our underpowered winch can overspeed the twins easily if the wind gets above about 15knots. If indicated airspeed is above 60knots, you're getting diminishing returns from the launch. Frank Whiteley |
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#4
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Dan G wrote: Should say that it's "full power all the way up" the main climb, of course we back off at the top. But there was some suprise at the launch point recently when a K21 waved off... the common thought was "K21s should be able to handle it". Maybe it could if it was no wind, but with a good headwind they just can't. And that was a surprise? Find yourself another club, man, because if headwinds on a winch launch are unexpected your current lot are going to damage someone one day. So far the sole answer to my original question has been "look at the wingtips during the launch and find what stick position will hold them at about 45 degrees to the horizon AND give a safe speed. If you have a low powered winch you may have to adopt a lesser angle" from Derek. Does everyone agree with this? No. I think it's bad advice. Yes, you should aim to have a proper climb angle and air speed, but the stick position is irrelevant. Just use enough to do what's needed. How many inches of rudder movement would you use to balance a 20 degree per second roll into a turn? Or would you just aim to us enough to keep the string straight? Ian |
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#5
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Hi Bill, Glad to see you are coming round to my way
of thinking, that the rotation into the full climb should be gentle and controlled, and should not put you in an unrecoverable position if the launch fails for any reason. The exact position to hold the stick during a winch launch is very type dependent. Gliders with way back c of g hooks, such as the K21, K8 and Pirat will require the stick to be held neutral or even forward of neutral during the full climb. Gliders with slightly further forward hooks such as the K13 will need the stick held fairly well back, although probably not on the back stop. Gliders with single 'compromise' hooks such as the Slingsby Skylark and the Bocian will need the stick to be held on the back stop if they are to climb at all steeply. The best advice I can give to Dan G is to look at the wingtips during the launch and find what stick position will hold them at about 45 degrees to the horizon AND give a safe speed. If you have a low powered winch you may have to adopt a lesser angle. Derek Copeland At 15:18 13 December 2006, Bill Daniels wrote: Dan, your questions concern me. Full up elevator is dangerous on a winch launch. All modern At 15:18 13 December 2006, Bill Daniels wrote: Dan, your questions concern me. Full up elevator is dangerous on a winch launch. All modern trainers like ASK 21's or Grob 103's will fly an almost perfect launch without the pilot touching the controls if trim and winch power are right. Demonstrating hands off launches is a good start to winch training. (The take home lession is the launch will be nearly perfect if the pilot doesn't screw it up.) You should be using just enough elevator to keep the airspeed where you want it. (Typically 55 - 60 knots, depending on the glider) The basic principle is that the winch driver controlls power and the glider pilot controlls airspeed. If it requires large amounts of up elevator to control airspeed, signal for less power. As you point out, some gliders with high CG locations like a K8 will need nearly full down elevator from the start to control the natural pitch up. It shouldn't need much up elevator at all later. The winch driver should be slowly backing off the power as the glider approaches the top of the launch. Take a good look at George Moores charts that show cable tension - tension is a direct function of winch power. In any event, there's very little additional height that can be achieved late in the launch. Pulling hard near the top just loads up the glider and may break the weak link. (You are using the correct Tost weak links, right?) Suggestion: Get a copy of a good glider flight simulator like Condor and practice lauches on a computer. There's a lot to learn with a good sim. I use Condor as an 'animated white board' when I teach winch ground school. Bill Daniels 'Dan G' wrote in message roups.com... Thanks Bill, that document is very interesting. There is one thing in particular I am unsure about however - how much up elevator I should be putting in. With the K8, I fly the launch at 50-55kts with the stick fully back for perhaps the last 30% of the launch after smoothly transitioning from full forwards on the ground run through neutral once in the full climb, until I feel the glider being pulled level, when I relax the aft pressure in anticipation of putting the nose down to reuce cable tension prior to releasing. (This later movement often results in quite an increase in speed, which I convert to height after releasing. Is this an indication I'm releasing back pressure too early, or the winch driver not backing off the throttle enough?) With a K21, which winch drivers here (which includes me) are told to give 'full power all the way up' from our Oldsmobile V8. Climb speed is at lesst 65kts and I'm reluctant to pull back too hard. Why? A K21 launches on a black weak link (1,000kg). I imagine full up elevator in a K21 would produce enough lift to break that at well below max winch speed, 81kts. Is there a way to calculate how much lifting force full up elevator should produce for any given airspeed? Or should I not be putting full up in? If not, just how far should I bring the stick back, and when? Bill Daniels wrote: If you join the Yahoo group 'winchdesign' and look in the files section, there are a series of truely excellent papers in the folder 'Winch Dynamics and Performance' by George Moore. (soargsm) Essentially what George determened is that the major sensitivities a 1.Field length 2. Headwind 3. Cable tension as a percentage of glider flying weight. 4. Weight & drag of the cable There is very little extra height to be gained by agressive technique beyond just hitting your target airspeed and holding it there with smooth control inputs. This gives an angle of attack just slightly greater than that for best L/D. If you want help with this, put some AOA strings on the canopy sides and calibrate them for L/D max and Vmin sink. Of course, it goes without saying that you should never put yourself in danger by rotating into the climb so quickly that a recovery from a rope break is impossible. Smooth and accurate flying are what you want. So, if you want to get higher, get a longer field with more wind, replace steel with high strength Dyneema and get a winch that can accurately hold tension at 80 - 90% of the weak link. Bill Daniels 'Dan G' wrote in message ups.com... I'm interested in learning how to get the maximum possible height on a winch launch, without compromising safety in any way. This question has two parts really - how should the pilot fly the launch (pretty much how should he operate the elevator during the launch), how fast should the glider fly, and how should the winch driver feed the power in? For the sake of argument, let's assume the glider is a K13. For reference, I fly from an airfield with a 3,300' long cable, and the maximum height I achieve repeatedly is 1,700'. Headwind typically goes from around 10kts at the ground to something like (I estimate) 20kts at height. |
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#6
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Derek Copeland wrote: The exact position to hold the stick during a winch launch is very type dependent. Gliders with way back c of g hooks, such as the K21, K8 and Pirat will require the stick to be held neutral or even forward of neutral during the full climb. My Pirat will fly a very nice winch launch which is almost completely independent of anything the pilot chooses to do with the stick! It's not so much the fore-and-aft position of the hook, I think, as the vertical one: since it is at the bottom of a deep fuselage there is a considerable nose up pitching moment during the ground run. As soon as it takes off, therefore, it does a lovely rotation into full climb all by itself: full forward stick has no effect at all. Gliders with single 'compromise' hooks such as the Slingsby Skylark and the Bocian will need the stick to be held on the back stop if they are to climb at all steeply. All the Bocians I have ever flown had C of G and nose hooks. The Pirat manual specifically permits winching on the nose hook: using full back stick and forward trim from the "All Out", and warning that it will only give 60% of normal release height. I have never tried this, for several reasons, one being that I rather like having the back release there ... Ian |
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#7
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#8
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Dan G wrote: Dan G wrote: how should the winch driver feed the power in? I received a very detailed reply in the Yahoo winch design group. With permission, I reproduce it below: Interesting ... but once more, beware of rules. Lots of factors can make differences to technique: whether the drive is direct, fluid flywheel or torque convertor, size of drums (and consequently inertia) and turbocharged vs normally aspirated. Ian |
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#9
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I have very little practical knowledge of winching and I
still do not understand what the theoretical factors are that determine max launch height. Neglecting wind speed and wind gradient for the moment, as well as safety concerns relating to rope breaks down low, what is the technique to max out height given the changing climb and tow line angles and geometry? Derek Piggot writes in his book "Ground Launches , 1996, pg 34.): “The optimum speed on the launch depends to some extent on the wind strength with a slightly higher speed giving the best launch height in calm conditions. Best L/D speed is close to the optimum, with the minimum cruising speed or speed for minimum sink being the lowest safe speed.” Derek Piggott, Ground Launches , 1996, pg 34. If the speed for best L/D is close to optimum, what is optimum? The American Soaring Handbook, Vol 3, Ground Launch, 1980, pg 32 says the following about auto tow “The factor which determines the towing speed of the automobile is the indicated air speed (IAS) of the sailplane. It has been shown that the launching forces on the sailplane are at a minimum just below the IAS for maximum L/D of the sailplane” Just how far below the best L/D IAS is the point of minimum stress on the airframe? Once we have derived the factors to max out launch height, how do you then balance efficiency versus climb rate after that point in the launch when you have enough altitude for a safe recovery from a low rope break? Pete -- Peter D. Brown http://home.gci.net/~pdb/ http://groups.yahoo.com/group/akmtnsoaring/ |
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#10
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Pete Brown wrote:
Derek Piggot writes in his book "Ground Launches , 1996, pg 34.): “The optimum speed on the launch depends to some extent on the wind strength with a slightly higher speed giving the best launch height in calm conditions. Best L/D speed is close to the optimum, with the minimum cruising speed or speed for minimum sink being the lowest safe speed.” Derek Piggott, Ground Launches , 1996, pg 34. If the speed for best L/D is close to optimum, what is optimum? The optimum is the best glide speed at the wing effective load factor based on the takeoff weight of the glider and the cable tension. For example, for an ASK-21 with a best L/D speed of 49 knots at a weight of 1300 lbs, if the cable tension is 1900 lbs, the effective load factor is 1950/1300 or 1.5, the optimum launch speed is 49*SQRT(1.5) or 60 knots IAS. The American Soaring Handbook, Vol 3, Ground Launch, 1980, pg 32 says the following about auto tow “The factor which determines the towing speed of the automobile is the indicated air speed (IAS) of the sailplane. It has been shown that the launching forces on the sailplane are at a minimum just below the IAS for maximum L/D of the sailplane” Just how far below the best L/D IAS is the point of minimum stress on the airframe? What they appear to be discussing here is a rule of thumb for automobile speed based on the non-adjusted best glide IAS of the glider. Given a nominal climb angle of 45 degrees, if the automobile is driving at 50 mph (44 knots), the glider will be flying at 62 knots TAS. So, in this case, once the glider has rotated to climb angle you'd want to drive 6 or 7 MPH slower than the gliders best L/D speed at sea level density altitude. If the density altitude is higher, you'd want to drive faster. Once we have derived the factors to max out launch height, how do you then balance efficiency versus climb rate after that point in the launch when you have enough altitude for a safe recovery from a low rope break? Assuming the winch (or automobile) is providing a constant cable tension, the max launch height will be pretty close to optimal if the pilot maintains the optimum launch speed IAS as calculated above. This should result in a climb angle for most of the launch of about 45 degrees. Marc |
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