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Forum: Tech Log
30th Jul 2006, 19:44
Replies: 4
Views: 2,946
Posted By Frank Poncherello

Assuming level flight, LIFT = WEIGHT,........... ...

Assuming level flight, LIFT = WEIGHT,...........

Lift Coefficient (CL) = L / (1/2 x rho x V^2 x S)

rho = density of air at sea level I guess (cant remember off hand, but might be something like...
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