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#11
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#12
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Gary and Eric, please don't get me wrong. I have the utmost respect for
both of you and the effort to understand the "superadiabatic layer". This is just a academic debate among friends. Just to set some credentials, 30 years ago I spent a lot of energy trying to solve the same problem. My approach was a 50 pound, 13 meter, 35:1 inflatable flying wing made of Kevlar reinforced Mylar that could be foot launched. The high pressure inflatable structure would have produced a highly accurate airfoil. I still think it would work, but the materials and construction techniques weren't available then. My legs are too old to even think of it now. Yes, Gary, I have seen vultures working boundary layer turbulence - it's fun to watch. I also noted that they don't make much progress against a 20 knot wind and that they posses an amazing landing and re-launch system if their microlift soaring efforts don't pay off. Low wing loading gliders working the same environment have the same problem moving upwind as the birds but lack the land and re-launch capability. At 200', it's easy to get out of range of a suitable landing spot. The low wing loading buys you the option of working microlift but it requires that you operate in a hostile environment where options are limited. At 200 feet with approximately one foot per second sink rate, you are three minutes from a forced landing if microlift fails. If I find myself in that situation, my most fervent wish is to get out of it - ASAP. Once out of it, I want a big, heavy glider to take advantage of better sources of energy found at higher altitudes. On the other hand, I strongly suspect that similar soaring possibilities exist at much higher altitudes and on a much larger scale. One problem in exploiting that energy is that a TE vario can't tell the difference between a thermal and a gust - plus it has a 2-3 second lag and a terrible signal-to-noise ratio. Develop an instrument that has instantaneous response plus the ability to resolve energy vectors in 3D and we may find there are many overlooked soaring possibilities that all gliders can use. Bill Daniels "Gary Osoba" wrote in message om... Bill Daniels wrote: If you fly at 10-12 pound wing loading in 15 knot thermals at 18000 feet, it's superfluous. Hello Bill: You are correct, a glider designed to optimize Microlift conditions would not be as well suited to cruising in these conditions. I, too, enjoy flying very heavy wing loadings in the strongest reasonable conditions. I am presently woking closely with Dr. Marsden on an experimental 15m racer which will ballast to 13 psf normally, and have designed a special system which would allow for 15 psf. This type of flying is very exciting, and a worthwhile area to explore and push the envelope. It is also ideally suited to pitch-based dynamic soaring with high inertias, something that mostly captivates my attention these days. However, there are other fields of endeavor which are also worthwhile. Have you ever stood on the ground in a 20 knot wind, and watched a vulture fly from horizon to horizon at an altitude of 200' - never once circling- against the wind? Ever wondered where is he getting this energy? Or which of the lateral movements he is constantly making are reactive and which ones are harvesting energy from random turbulence? Some of us find this simple scenario at least as interesting and exciting as the former one. At the very least, we would like to understand it better and at the most, emulate or even exceed it. This is one (and only one) of the things that Microlift optimized designs are capable of doing which higher W/S approaches do not. As it turns out, there are not simply quantitative differences which are taking place at lower altitudes in the convecttive environment but qualitative ones as well. The near-earth environment does not simply contain thermal plumes which are lower than those normally encountered in soaring flight at higher altitudes. There are structural differences between the super-adiabatic layer, the next mixed layer, and the higher normal soaring environment. Scale is important here. The size of less organized structures which are not yet thermal plumes in these lower environments is not well suited to a 12 psf W/S glider, or even a 6 spf one. Likewise, the magnitude of stochastic but often widespread gusting and turbulence may comprise a large fraction of the total flight energy of a low inertia glider, whereas its nothing more than an annoyance in higher inertia systems. With proper coordination and flight maneuvering, these smaller turbulent events can impart repeating and substantial amounts of energy to flight systems. However, the systems used must be matched to the environment and it is not simply a function of wing loading. The entrained air mass of the flying system, which is a function of not only W/Sbut also mac and other factors must be considered. Manueverability is very important, particularly rolling responses. Until you have experienced this, it his hard to appreciate how it could be as exciting as cruising at redline and 18k north of Tonopah, while still 5k *under* cloudbase. However, I find it to be at least as exciting. Not as high. Not as fast. But somehow just as amazing. Not better. Not worse. Different, Bill. Something new to explore, which is very, very old. I guess it could be stated another way. I have never had the opportunity to watch the launch of the Space Shuttle. I would like to. However, if I had unlimited opportunity I suppose I would tire of it after enough times. I don't beilieve I will ever tire of watching vultures, or sea gulls, or even butterflies doing their thing. Still skeptical. That's your prerogative. I would prescribe a little more time for direct observation of the natural world, and a little less time trying to view it as it rapidly recedes in your high speed rear-view mirror. Best Regards, Gary Osoba |
#13
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Eric Greenwell wrote in message ...
Maybe, if you flew a LightHawk in the conditions it was designed for, you'd also be less skeptical. I'd like to give it a try. I'm kinda with Bill on this. Microlift sounds like fun, a good way to fly on days that won't support heavier gliders - but the thought of going crosscountry at low altitudes and low speeds, even if you can land in anyone's backyard, just doesn't appeal to me very much. If it did, I would be flying a hang glider or paraglider. And microlift soaring is going to be a pretty intense activity - not much time to relax and cruise along when you are low most of the time, or your L/D at higher speeds is going to put you low again soon. Nothing wrong with that (as the success of the 1-26 proves) but not everybody's cup of tea. The problem I see is that the cost of a high tech microlift glider is going to be very close to a "conventional lift" glider, but the utility will be a lot less - in that the range I can cover in available time is a lot less. And how is that low wingloading going to handle those fun windy. booming days? When the cloud steets are kicking up 10 knots, and you are looking at a 30 knot headwind for your 70 mile final glide...I think I want to have my nice heavy wingloading, thankyou. So if you want to see the same ground from up close, then go for it. I think I prefer to see more ground from up high! Another problem I see is in enticing people to go XC in microlift gliders - sure a confident pilot will set off at 1000ft expecting to find more microlift to keep going, out of range of any airfield, in his $30k+ Microhawk; but your average Twirlybird is scared to death of getting out of 10/1 from the home gliderport - he is never going to push out at those altitudes - it's just too scary for him! Anyway, keep up the good work - you guys are essentially filling the gap between hang/paragliders and heavy gliders, and that is a good thing, since in some areas (and for some pilots) that is exactly what is needed. Kirk |
#14
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Bill Daniels wrote:
Low wing loading gliders working the same environment have the same problem moving upwind as the birds but lack the land and re-launch capability. At 200', it's easy to get out of range of a suitable landing spot. THis is very dependent on where you fly. How about Kansas? Or here in Eastern Washington State, were the fields are a mile square, half of them fallow, half of the other half in low crops, and cover hundreds of square miles at a stretch. They are prolific producers of low lift on many days. The low wing loading buys you the option of working microlift but it requires that you operate in a hostile environment where options are limited. Not! See above. At 200 feet with approximately one foot per second sink rate, you are three minutes from a forced landing if microlift fails. I think you grab should hold of this microlift idea because the gliders are ideal candidates for one of your preferred launch methods: winch launching. THese gliders require only a small, low powered winch, and to low altitudes (500', say). An airport isn't required. -- ----- change "netto" to "net" to email me directly Eric Greenwell Washington State USA |
#15
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When Microlift conditions go bad, is the lift then called microsoft?
- Mark Navarre ASW-20 OD California, USA - |
#16
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"Mark Navarre" wrote in message ... When Microlift conditions go bad, is the lift then called microsoft? - Mark Navarre ASW-20 OD California, USA - Oh no! Gates will now patent and copyright microlift and each of us will have to pay a licence fee per thermal. Every 2 years the thermals will get an upgrade and will cost more, the hardware required to exploit them will need to be more and more sophisticated but wont actually do anything new. :-) Ian |
#17
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The thermals might be restored by opening and closing the windows.
-- Gary Boggs 3650 Airport Dr. Hood River, Oregon, USA 97031-9613 "tango4" wrote in message ... "Mark Navarre" wrote in message ... When Microlift conditions go bad, is the lift then called microsoft? - Mark Navarre ASW-20 OD California, USA - Oh no! Gates will now patent and copyright microlift and each of us will have to pay a licence fee per thermal. Every 2 years the thermals will get an upgrade and will cost more, the hardware required to exploit them will need to be more and more sophisticated but wont actually do anything new. :-) Ian |
#18
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Kind of like buying a new car every two years because Detroit changes the
fenders or someone makes one that is called a SUV and every person in town has to have one. If you don't like Microsoft, try doing your business without the world of computers that they have assisted in creating. Without MS, you would not have money to buy all the glider toys you play with every weekend. "tango4" wrote in message ... "Mark Navarre" wrote in message ... When Microlift conditions go bad, is the lift then called microsoft? - Mark Navarre ASW-20 OD California, USA - Oh no! Gates will now patent and copyright microlift and each of us will have to pay a licence fee per thermal. Every 2 years the thermals will get an upgrade and will cost more, the hardware required to exploit them will need to be more and more sophisticated but wont actually do anything new. :-) Ian |
#19
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On Mon, 8 Mar 2004 06:51:54 -0800, "Libelle Driver"
wrote: Kind of like buying a new car every two years because Detroit changes the fenders or someone makes one that is called a SUV and every person in town has to have one. If you don't like Microsoft, try doing your business without the world of computers that they have assisted in creating. Without MS, you would not have money to buy all the glider toys you play with every weekend. Actually, that's quite easy: throughout my professional life I have never used a DOS or Windows PC for more than a cheap terminal and word processor. Now, thanks to Linux and Open Office I can do everything quite nicely, thanks, without any of Mr Gates' products. -- martin@ : Martin Gregorie gregorie : Harlow, UK demon : co : Zappa fan & glider pilot uk : |
#20
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Gary Osoba wrote:
at Lausanne, Switzerland, had voted to accept the OSTIV-proposed definition and creation of a new class of gliders- MIcrolift. .... of micro-interest :-((( -- Denis R. Parce que ça rompt le cours normal de la conversation !!! Q. Pourquoi ne faut-il pas répondre au-dessus de la question ? |
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