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On Jan 4, 12:58*am, "
wrote: On Jan 3, 6:30*pm, ProfChrisReed wrote: It seems to me that increased AoA must be a very large part of the cause. Imagine you are flying free @55kt. You have a sink rate of, say, 1.5kt. Now you are on tow, again @55kt, but this time the combination is climbing @5kt. Your wings are generating 6.5kt more lift than in free flight, and must therefore be at a substantially higher AoA. Additionally, the faster you are climbing (in still air) the greater the AoA must be for you to keep station with the tug. I fly an Open Cirrus, towing from the C of G hook without ballast, and never experienced this at my previous club which had a Citabria tug. My current club has a Pawnee, and I have from time to time felt the tow was too slow because the controls felt mushy and the glider wallowed about, feeling as if it was close to the stall. The Pawnee climbs much faster than the Citabria. If in addition the tug's slipstream imparts a downward flow to the airmass, even more lift and higher AoA is required. Actaully, comparing climbing steeply say, 10:1 on tow, to gliding at 40:1, *the lift vector is (a tiny bit) SMALLER during the tow! During the 10:1 tow, lift would be 99.5% of the glider's weight, while during a 40:1 glide, lift would be 99.97% of the glider's weight! (the missing 0.5% on tow is made up by the thrust vector...the missing 0.03% in glide is made up by the drag vector. Cookie Cookie- Hide quoted text - - Show quoted text - If you had a really powerful tug that was capable of climbing vertically, then the glider would just be dangling on the end of the rope and would not have to produce any lift. The tension in the rope would be equal to the weight of the glider plus any drag components. While this is not a very likely scenario, I do think that the thrust vector must be greater in a 10% climb than you are claiming. Derek C |
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