(1)t=L/v0
0.5at*t=h==>a=2h/t^2=2hv0^2/L^2
F-mg=ma==>F=mg+2mhv0^2/L^2
(2)升力所的功=Fh=h(mg+2mhv0^2/L^2)
离度h处飞机的动能=0.5mv0^2+升力所的功-克服重力所做的功=0.5mv^02+2mh^2v0^2/L^2
(1)t=L/v0
0.5at*t=h==>a=2h/t^2=2hv0^2/L^2
F-mg=ma==>F=mg+2mhv0^2/L^2
(2)升力所的功=Fh=h(mg+2mhv0^2/L^2)
离度h处飞机的动能=0.5mv0^2+升力所的功-克服重力所做的功=0.5mv^02+2mh^2v0^2/L^2