Prove that the components of the orbital angular momentum satisfy [L, p²] = [L‚,p²] = ô, j=x,y,z where p2 = £2 + ŷ² + 2² _y p² = p% + p3 + p² .
Prove that the components of the orbital angular momentum satisfy [L, p²] = [L‚,p²] = ô, j=x,y,z where p2 = £2 + ŷ² + 2² _y p² = p% + p3 + p² .
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