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Forum: Tech Log
29th Nov 2010, 11:46
Replies: 3
Views: 1,853
Posted By s2679243

Thanks so much! makes sense now! :)

Thanks so much! makes sense now! :)
Forum: Tech Log
29th Nov 2010, 09:26
Replies: 3
Views: 1,853
Posted By s2679243

Calculating IAS from lift equation

Hi,
Given Cl = 0.2, Weight of aircraft = 170 tonnes and Smainwing = 250m^2 and Stailwing = 56m^2 is it possible to calculate the IAS (in km/hr) the aircraft should travel so that L = W ?

I am...
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