Conservation of Energy - Statics and Dynamics

  1. What is the minimum value of E0E_0 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: E0=2mgRE_0 = 2mgR, because the bead only needs enough energy to reach the top of the loop (height 2R2R) 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 vtop2≥gRv_{top}^2 \geq gR 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 vtop=0v_{top} = 0, and energy conservation gives: E0=ΔPE=mg(2R)E_0 = \Delta PE = mg(2R) So the minimum initial kinetic energy is E0=2mgRE_0 = 2mgR, confirming answer A. Answer B applies the condition mg=mvtop2/Rmg = mv_{top}^2/R, 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 E0E_0. 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 RR instead of 2R2R, a geometric error — the top of a loop of radius RR is at height 2R2R 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.
  2. After the rod catches on the peg, what is the minimum distance dd 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: d=L−L2=L2d = L - \frac{L}{2} = \frac{L}{2}, because for a rigid rod the bob only needs to reach the top of the new loop with zero velocity, requiring (L−d)=L/2(L-d) = L/2 to satisfy the energy balance mgL=mg⋅2(L−d)mgL = mg \cdot 2(L-d). 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 vtop2≥g(L−d)v_{top}^2 \geq g(L-d). A rigid rod, however, can push as well as pull — meaning the bob only needs to arrive at the top with vtop≥0v_{top} \geq 0. 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 LL from its release point, giving it kinetic energy 12mv2=mgL\frac{1}{2}mv^2 = mgL. After catching the peg, the bob must rise a height 2(L−d)2(L-d) to reach the top of the new loop. Setting energy equal to zero velocity at the top: mgL=mg⋅2(L−d)mgL = mg \cdot 2(L-d), which gives L=2(L−d)L = 2(L-d), so L−d=L2L - d = \frac{L}{2} and d=L2d = \frac{L}{2}. Answer B applies the string condition vtop2=g(L−d)v_{top}^2 = g(L-d) 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 d=3L5d = \frac{3L}{5}. Answer C misidentifies the geometry, treating dd as the new effective length rather than (L−d)(L-d). 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 → vtop=0v_{top} = 0 is sufficient; String → vtop2≥gℓv_{top}^2 \geq g\ell is required.
  3. Using conservation of energy and the vis-viva equation, what is the semi-major axis aa of the new elliptical orbit? Recall that for any orbit the total mechanical energy is E=−GmpM/(2a)E = -Gm_pM/(2a).
    Answer: a=R2−R(v0−Δv)2/(Gmp)a = \frac{R}{2 - R(v_0 - \Delta v)^2/(Gm_p)}, obtained by setting the total energy after the burn equal to −GmpM/(2a)-Gm_pM/(2a) and solving for aa. 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 E=KE+PEE = KE + PE can be equated to the orbital energy formula E=−GmpM/(2a)E = -Gm_pM/(2a), letting you solve directly for the semi-major axis aa. Right after the burn, the spacecraft is still at radius RR, so its potential energy is unchanged at −GmpM/R-Gm_pM/R. Its kinetic energy is now 12M(v0−Δv)2\frac{1}{2}M(v_0 - \Delta v)^2. Setting the total energy equal to −GmpM/(2a)-Gm_pM/(2a): 12M(v0−Δv)2−GmpMR=−GmpM2a\frac{1}{2}M(v_0-\Delta v)^2 - \frac{Gm_pM}{R} = -\frac{Gm_pM}{2a} Dividing through by MM, rearranging, and solving for aa yields: a=R2−R(v0−Δv)2/(Gmp)a = \frac{R}{2 - R(v_0-\Delta v)^2/(Gm_p)} 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 Δv=0\Delta v = 0, you recover a=Ra = R), but it doesn't answer the question for nonzero Δv\Delta v — 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 MM 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 MM early when working orbital energy problems — if MM survives to the final answer for aa, something has gone wrong.

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