On the Earth
T=2πlg→l=gT24π2=9.81⋅224⋅3.142≈1(m)T=2\pi\sqrt{\frac{l}{g}}\to l=\frac{gT^2}{4\pi^2}=\frac{9.81\cdot2^2}{4\cdot3.14^2}\approx1(m)T=2πgl→l=4π2gT2=4⋅3.1429.81⋅22≈1(m)
On the Moon
T=2πlg→l=gT24π2=T=2\pi\sqrt{\frac{l}{g}}\to l=\frac{gT^2}{4\pi^2}=T=2πgl→l=4π2gT2=
=(9.81/6)⋅224⋅3.142≈0.166(m)=\frac{(9.81/6)\cdot2^2}{4\cdot3.14^2}\approx0.166(m)=4⋅3.142(9.81/6)⋅22≈0.166(m)
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