Lift during climb calculator

In flight mechanics, “lift during climb” refers to the aerodynamic force that supports an aircraft’s weight as it ascends at a specific rate of climb while flying at a particular airspeed and altitude. Lift during climb is essential for maintaining the aircraft’s vertical motion and rate of ascent.
Lc=(1-Vc^2/v^2)
Vc means rate of climb
v means velocity

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