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![]() "Andy Durbin" wrote in message om... (Chris OCallaghan) wrote in message om... Well, at least we've got everyone on the same theme now. It's the drag. Why don't you guys in Phoenix do a little testing and we'll do the same here at M-ASA. I think we all agree that the heavier glider has a significant drag advantage at high speed, and will gain additional altitude. But how much, exactly? So far I have not seen anyone consider the fact that, at the same (high) speed, the unballasted glider has a significantly higher sink rate at the start of the pull up. The initial conditions are not the same. Andy (GY) The sink rate for the fully loaded glider(190 litres) = 1.2m/s for the none ballaste version 1.65m/s Udo |
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Udo Rumpf wrote:
The sink rate for the fully loaded glider(190 litres) = 1.2m/s for the none ballaste version 1.65m/s And the vertical kinetic energy converted to altitude (the only place where we can take the energy in a glider) would be h=v^2/(2g) so for 1.2 and 1.65 m/s the altitude losses would be 0.073 and 0.139 m respectively. Not a signifigant factor I would say. Plus, we would have to take into account the fact that in the end as well (after levelling out) their sink rates will be different. But still no signifigant effect... Jere jere at iki.fi |
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