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 calculating velocity)
but as i got old i don't remember.
any idea ?