Recent content by thekacker

i'm such a kacker long days guys too long of a day

Lift=weight=mg=clqS ? q as in dynamic pressure ? and mg ? what's that ?

i know what the formula is airplane mass : 60,000 Kg acceleration of gravity is 9.81 m/(s*s) wing area is 105 m*m density is standard icao value 1.225 kg/m*m*m and Cl = 0.384 how do i find L from the above. i think it has to do with finding acceleration (force / mass) and then from that...

guys i remember the lift equation to be L= 1/2 rho V*V Cl S i need to calculate V i have rho i have cl and i have S and i don't remember how to do that