Question 6 of 6: Diffraction-limited focal spot, a two-wavelength double slit, an anti-reflection coating, and a moving mirror
Nivaar worked solution (AI-drafted; not reviewed by a licensed engineer)
Notes on this paper
Paper format. National Examinations, December 2013, 98-Phys-A7 Optics. Three hours, closed book, one approved Casio or Sharp calculator. Question 1 (20 short parts) is mandatory; the rubric asks for any four of Questions 2–6 — all six are worked here, because the set is a study resource.
Reference texts. E. Hecht, Optics, 5th ed.; F. L. Pedrotti, L. M. Pedrotti and L. S. Pedrotti, Introduction to Optics, 3rd ed.
Question 6: Diffraction-limited focal spot, a two-wavelength double slit, an anti-reflection coating, and a moving mirror (20 marks)
Part (a). Given. Circular lens, f/#=5, f=10 cm (so D=2 cm), point source at 20 cm in front of the lens.
Huygens–Fresnel construction: every point of the circular aperture radiates a secondary wavelet; their coherent sum in the image plane is the Airy pattern, a bright central disc surrounded by faint rings.
Huygens–Fresnel principle. Every point of the illuminated circular aperture is treated as a source of a secondary spherical wavelet; the field at a point in the focal plane is the coherent (phase-correct) sum of all these wavelets, i.e. the Fraunhofer diffraction integral of the circular aperture. For a circular aperture this integral is the Airy function $I(v)=I_0\left[2J_1(v)/v\right]^2$.
Working f-number. The source is not at infinity, so the relevant cone angle is set by the actual image conjugate: $\dfrac1{d_i}=\dfrac1f-\dfrac1{d_o}=\dfrac1{10}-\dfrac1{20}=\dfrac1{20}\Rightarrow d_i=20$ cm ($m=-1$), so the working f-number is $N_{eff}=d_i/D=20/2=\boxed{10}$ (twice the nominal f/5, as expected for unit magnification, $N_{eff}=(f/\#)(1+|m|)$).
Airy-disc dimensions. The first dark ring sits at $r_1=1.22\,\lambda\,N_{eff}=12.2\,\lambda$ and the second dark ring at $r_2=2.23\,\lambda\,N_{eff}=22.3\,\lambda$ (no source wavelength is given, so these are left proportional to $\lambda$); illustratively, at $\lambda=550$ nm, $\boxed{r_1\approx6.7\ \mu\text{m}}$, $r_2\approx12.3\ \mu$m, with the first bright ring only about 1.75% as intense as the central peak.
Check: no wavelength is given in the source for part (a); λ=550 nm is used only to illustrate the ring size numerically. The dimensions above scale linearly with whatever λ is used.
Part (b). Given. $\lambda_1=500$ nm; minima at $d\sin\theta=(k-\tfrac12)\lambda$, $k=1,2,\dots$; maxima at $d\sin\theta=n\lambda$, $n=0,1,2,\dots$ (central fringe not counted as the “1st maximum”).
Coincidence condition. 4th minimum of 500 nm: path difference $\Delta=(4-\tfrac12)(500\text{ nm})=1750$ nm. 3rd maximum of the unknown line: $\Delta=3\lambda\prime$. Equating, $$\lambda\prime=\frac{1750}{3}=\boxed{583.3\text{ nm}}$$
Part (c). Given. $n_{sub}=1.50$, $\lambda=600$ nm, normal incidence.
Single-layer AR coating: reflections r1 (top surface) and r2 (coating/substrate interface) are equal in magnitude and 180° out of phase, cancelling.
Coating index. Zero reflection requires the two surface reflections (air/coating and coating/substrate) to have EQUAL magnitude, which for normal incidence needs $$n_{coat}=\sqrt{n_{air}\,n_{sub}}=\sqrt{(1.00)(1.50)}=\boxed{1.2247}$$
Coating thickness. The two reflections must also be 180° out of phase, which for the thinnest (quarter-wave) coating gives $$t=\frac{\lambda}{4\,n_{coat}}=\frac{600\text{ nm}}{4(1.2247)}=\boxed{122.5\text{ nm}}$$
Part (d). Given. Normal incidence, mirror speed $v\ll c$ along the beam direction.
Double Doppler shift. Reflection from a moving mirror is equivalent to two successive Doppler shifts — once as the mirror “receives” the wave, once as it “re-emits” it. For $\beta=v/c\ll1$ the two first-order shifts add: $$\boxed{\frac{\Delta f}{f}\approx\pm\frac{2v}{c}}\ ,\qquad \boxed{\frac{\Delta\lambda}{\lambda}\approx\mp\frac{2v}{c}}$$ (upper sign: mirror approaching the source → blueshift, wavelength decreases; lower sign: mirror receding → redshift), exactly twice the single-source Doppler shift because the path length itself is changing at rate $2v$.