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Search: Posts Made By: WeekendFlyer
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Forum: Tech Log
31st May 2013, 22:00
Replies: 29
Views: 34,409
Posted By WeekendFlyer

A few thoughts on CL and stall

Sometimes it helps to use the equations:

Lift = nW = 0.5 * density * wing area * speed^2 * CL

where n = load factor (number of g) and W = weight = mass x gravitational acceleration

Put...
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