Discovering the Nucleus — Question 7

Section 42-1 · Physics pages 7004–7005

Question 7 Finite impact parameter raises the closest-approach distance A projectile of mass m, asymptotic speed v and impact parameter b scatters from a fixed repulsive center with potential K/r. Define E = mv2/2 and a = K/(2E). +Ze b θ Schematic; labels, not drawing lengths, specify the data. (a) Use conservation of energy and angular momentum to derive rmin. (b) For a = 10.0 fm and b = 24.0 fm, calculate rmin and compare with the head-on value.
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Question 7 - Solution Finite impact parameter raises the closest-approach distance +Ze b θ (a) Method and calculation L = mvb, E = L2 2mr2 min + K rmin ⇒r2 min −2armin −b2 = 0. rmin = a + √ a2 + b2 . (b) Interpretation and further calculation rmin = 10 + √ 100 + 576 = 36.0 fm . b = 0 : rhead = 2a = 20.0 fm, rmin/rhead = 1.80 . Physical check Radial speed vanishes at closest approach, but tangential speed generally does not. Setting all kinetic energy to zero would be valid only for a head-on orbit.

Question 7

Finite impact parameter raises the closest-approach distance

A projectile of mass m, asymptotic speed v and impact parameter b scatters from a fixed repulsive center with potential K/rK/r. Define E=mv2/2E=mv^2/2 and a=K/(2E)a=K/(2E).

Diagram shown in the original SVG worksheet.

  1. Use conservation of energy and angular momentum to derive rminr_{\min}.

  2. For a=10.0fma=10.0\,\mathrm{fm} and b=24.0fmb=24.0\,\mathrm{fm}, calculate rminr_{\min} and compare with the head-on value.

Question 7 - Solution

Finite impact parameter raises the closest-approach distance

Diagram shown in the original SVG worksheet.

(a) Method and calculation

L=mvb,E=L22mrmin⁡2+Krmin⇒rmin⁡2−2armin−b2=0.L=mvb,\quad E=\frac{L^2}{2mr_{\min}^2}+\frac K{r_{\min}}\Rightarrow r_{\min}^2-2ar_{\min}-b^2=0.rmin=a+a2+b2.\boxed{r_{\min}=a+\sqrt{a^2+b^2}}.

(b) Interpretation and further calculation

rmin=10+100+576=36.0fm.\boxed{r_{\min}=10+\sqrt{100+576}=36.0\,\mathrm{fm}}.b=0:rhead=2a=20.0fm,rmin/rhead=1.80.b=0:\quad\boxed{r_{\mathrm{head}}=2a=20.0\,\mathrm{fm},\quad r_{\min}/r_{\mathrm{head}}=1.80}.

Physical check

Radial speed vanishes at closest approach, but tangential speed generally does not. Setting all kinetic energy to zero would be valid only for a head-on orbit.