Conservation of Energy - Statics and Dynamics
- What is the minimum value of required for the bead to maintain contact with the loop at the very top? Note that for a bead on a wire (as opposed to a ball on a track), the wire can exert both inward and outward normal forces on the bead. Answer: , because the bead only needs enough energy to reach the top of the loop (height ) with zero speed, since the wire can pull the bead inward if needed. When a bead is threaded on a wire loop, the wire can exert forces in both directions — inward and outward — unlike a ball on a track that can only be pushed inward by the surface. This distinction completely changes the minimum energy condition. For a ball on a frictionless track, contact is lost when the normal force drops to zero, requiring at the top. But for a bead on a wire, the wire can pull the bead inward (like a tension), so the bead stays on the loop regardless of speed — even at zero speed. The only requirement is that the bead physically reaches the top. Therefore, the minimum condition is simply , and energy conservation gives: So the minimum initial kinetic energy is , confirming answer A. Answer B applies the condition , which is the constraint for a ball on the inside of a track — not a bead on a wire. It incorrectly assumes the normal force can only push inward, leading to an unnecessarily large . Answer C attempts an algebraic manipulation but starts from the wrong physical premise (the ball-on-track condition), so its "contradiction" is self-inflicted rather than revealing. Answer D misidentifies the height gained at the top as instead of , a geometric error — the top of a loop of radius is at height above the bottom. Key tip: Always ask whether the constraint is one-sided (track) or two-sided (wire/rod). A bead on a wire or a ball on a rod changes the minimum speed condition dramatically — often dropping it to zero.
- After the rod catches on the peg, what is the minimum distance such that the bob completes a full circular loop around the peg? Assume the rod is rigid (can push and pull), not a string. Answer: , because for a rigid rod the bob only needs to reach the top of the new loop with zero velocity, requiring to satisfy the energy balance . When a pendulum problem involves a rigid rod (not a string), the critical distinction is what condition must be met at the top of the loop. A string requires centripetal tension, so . A rigid rod, however, can push as well as pull — meaning the bob only needs to arrive at the top with . This single insight unlocks the whole problem. Answer A is correct. At the moment the rod catches the peg (the lowest point), the bob has fallen a height from its release point, giving it kinetic energy . After catching the peg, the bob must rise a height to reach the top of the new loop. Setting energy equal to zero velocity at the top: , which gives , so and . Answer B applies the string condition to a rigid rod — this is the most common trap. Because the rod can push, you don't need any nonzero speed at the top, making B's derivation unnecessarily restrictive and yielding the wrong . Answer C misidentifies the geometry, treating as the new effective length rather than . This is a setup misread that produces a completely incorrect energy equation. Answer D mixes the rigid-rod energy condition with leftover centripetal terms from the string case — a hybrid error that fits neither scenario. Study tip: Always identify whether the pendulum uses a rod or string first, since this determines your condition at the top. Rod → is sufficient; String → is required.
- Using conservation of energy and the vis-viva equation, what is the semi-major axis of the new elliptical orbit? Recall that for any orbit the total mechanical energy is . Answer: , obtained by setting the total energy after the burn equal to and solving for . When a spacecraft changes speed, its total mechanical energy changes, and that new energy uniquely determines the shape of the resulting orbit. The key tool here is recognizing that total mechanical energy can be equated to the orbital energy formula , letting you solve directly for the semi-major axis . Right after the burn, the spacecraft is still at radius , so its potential energy is unchanged at . Its kinetic energy is now . Setting the total energy equal to : Dividing through by , rearranging, and solving for yields: This is exactly answer A — the correct result, cleanly derived by applying energy conservation with the actual post-burn speed. Answer B is a useful sanity check (when , you recover ), but it doesn't answer the question for nonzero — it simply ignores the burn altogether. Answer C contains a critical sign error: the kinetic energy term appears with a positive sign in the denominator instead of negative, which would imply a larger orbit when the spacecraft actually slows down and falls inward. Answer D retains in both numerator and denominator in a way that cancels incorrectly, producing an expression that looks dimensional but doesn't reduce to the standard vis-viva form. As a study tip: always cancel early when working orbital energy problems — if survives to the final answer for , something has gone wrong.