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On Dec 8, 12:46*pm, CLewis95 wrote:
from Paul (sisu1a): ..... *But as I understand it, the pressure at the tail is kinda on a ship by ship basis. Some ships even suck water up the tailpipe when blowing ballast, which is a pretty good indicator of a poor choice for a 'low pressure' location. ... Paul (ALL) I have this problem with my Genesis 2 (both water and "other" fluids). Does this come from a "venturi" effect of air leaking from Horz/Vert Stab Junction or poor Rudder Sealing? *It amazes me how much gets sucked back into fuselage. *(Genesis has VERY short fuselage) Another Genesis owner (DK) has experimented with an exit duct out the fuse hatch over wings. ... comments Don??? Curt - 95 Likely due to pressure recoveing over the very short length of fuselage and large reduction in cross section over that length. High location closer to centerline would probably better in order to avoid effects on root fillet area. Just speculating- It's cold here. UH |
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![]() I have this problem with my Genesis 2 (both water and "other" fluids). Does this come from a "venturi" effect of air leaking from Horz/Vert Stab Junction or poor Rudder Sealing? *It amazes me how much gets sucked back into fuselage. *(Genesis has VERY short fuselage) Another Genesis owner (DK) has experimented with an exit duct out the fuse hatch over wings. ... comments Don??? Curt - 95 I have had an air outlet on my Genesis2 for several years. It was modeled after the outlet on DB's ASW-22. It seems to work very well. Curt is correct that on a Genesis 2, dumped water ballast will enter the fuselage thru the fairings over the rudder horns. These fairings are suppose to be the air outlets. I have taken photos of that area with tufts taped around the fairings. And indeed the tufts turn and are sucked into the "outlets". Don (DK) |
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On Dec 7, 10:46*am, Mike the Strike wrote:
On Dec 7, 7:56*am, Andy wrote: On Dec 6, 7:37*pm, sisu1a wrote: http://tinyurl.com/337bok7**...I'm sure it works like a champ. *Nice work John/Hank/Dick! Looks nice but where do I put all the stuff that now sits in the over- spar storage area? *I don't think I want to discard my landout kit so I can fit a vent system that has an unknown (to me) performance advantage. For me to be interested in a kit for the ASW-28 it would have to extend the storage area aft so that, with the vent kit installed, at least the same storage volume was still available, preferably more. There is lots of room to extend backwards as is done in the 27's. Unlike shorter pilots there in no room behind my seat and everything I carry has to go just forward of, or over the spar. Where can I find a picture of the installation looking aft into the spar area? Andy An interesting gadget. *However, wouldn't it be more logical to vent nearer the rear of the fuselage, say in the lower tail? Mike- Hide quoted text - - Show quoted text - I have an exit vent in the lower aft area of the fuselage of both my '27 and '28. With all the other stuff done sealing rudder hinge, elevator drive, horn splitters, etc, it improved negative pressure and flow and resulted in less noise. This vent is a huge ass ache to put in with the associated nozzle, has significant structural implications requiring reinforcement, and simply, is not for the faint hearted. The new vent on top is in a low pressure area which helps a lot with getting flow and reduced cockpit pressure. It also takes an hour and a half to install instead of about 10 hr. It's structural implications are minimal. It slightly reduces available baggage storage in the top center 4 inches. Both my gliders will have rear vents closed this winter and '28 will get top vent. FWIW UH |
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In article ,
Don Johnstone wrote: Do you blokes suffer from major flatulence problems? Seems a lot of effort to remove air from the cockpit but I could understand if the air was contaminated in some way :-) Around here (northern Virginia) there's a month or two of summer where I spend pretty much the entire flight with my hand stuck outside to get as much air in as possible to try to stay cool. On one miserably hot day this past July I had to cut a flight short as I began to seriously overheat despite all my best efforts. I have one of Paul's extractors on order and I'm hoping it'll make next summer much more pleasant. -- Mike Ash Radio Free Earth Broadcasting from our climate-controlled studios deep inside the Moon |
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On Dec 7, 12:47*pm, Don Johnstone wrote:
Do you blokes suffer from major flatulence problems? Seems a lot of effort to remove air from the cockpit but I could understand if the air was contaminated in some way :-) At issue is that ventilation air tends to pressurize the cockpit, and then leak out around the canopy perimeter. Anywhere that there is air escaping through the canopy frame gap, that leak will trip the boundary layer and increase drag. If you can keep the cockpit at lower than ambient pressure, you run a good chance of maintaining laminar flow across the gap between the fuselage and the canopy, which can result in several more square feet of laminar flow than you had previously. I happen to think that many original designers got it right; that the most effective vent is back at the base of the rudder, where it is convenient to exhaust air around the rudder cable horns. Unfortunately, something often got lost in translation, and most production gliders allow too little exhaust area through the vertical fin spar, causing inadequate ventilation flow and too much cockpit pressure. They also offer many restrictions on the path from the cockpit to the tailboom, which reduces the flow rate. So I think that these trendy exhaust vents, while perhaps not the best possible solution, are still a lot better than you can get without removing the rudder and doing some relatively major surgery on the fin spar. Thanks, Bob K. http://www.hpaircraft.com |
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On Dec 8, 11:20*am, Bob Kuykendall wrote:
On Dec 7, 12:47*pm, Don Johnstone wrote: Do you blokes suffer from major flatulence problems? Seems a lot of effort to remove air from the cockpit but I could understand if the air was contaminated in some way :-) At issue is that ventilation air tends to pressurize the cockpit, and then leak out around the canopy perimeter. Anywhere that there is air escaping through the canopy frame gap, that leak will trip the boundary layer and increase drag. If you can keep the cockpit at lower than ambient pressure, you run a good chance of maintaining laminar flow across the gap between the fuselage and the canopy, which can result in several more square feet of laminar flow than you had previously. I happen to think that many original designers got it right; that the most effective vent is back at the base of the rudder, where it is convenient to exhaust air around the rudder cable horns. Unfortunately, something often got lost in translation, and most production gliders allow too little exhaust area through the vertical fin spar, causing inadequate ventilation flow and too much cockpit pressure. They also offer many restrictions on the path from the cockpit to the tailboom, which reduces the flow rate. So I think that these trendy exhaust vents, while perhaps not the best possible solution, are still a lot better than you can get without removing the rudder and doing some relatively major surgery on the fin spar. Thanks, Bob K.http://www.hpaircraft.com .... and as JS pointed out, many of us fly where it is REALLY hot, with ambient temperatures of 43c, 110f, and closed cockpit temperature over 55c, 130f. It doesn't take long at that temperature to ruin an otherwise great flying day. |
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What keeps rain, wasps, mice, etc. from entering the vent hole when on
the ground? |
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On Dec 9, 3:11*am, "Matt Herron Jr." wrote:
What keeps rain, wasps, mice, etc. from entering the vent hole when on the ground? We don't have mice running around on our launch grid and rarely grid in the rain. Guess I just didn't think about those problems. UH |
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At 08:11 09 December 2010, Matt Herron Jr. wrote:
What keeps rain, wasps, mice, etc. from entering the vent hole when on the ground? Canopy cover? |
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