Question 4 of 4: Radiation Exchange Between a Heater and a Conical Shield
Nivaar worked solution (AI-drafted; not reviewed by a licensed engineer)
Notes on this paper
National Exams — May 2018 — 04-Agric-A3 Heat Engineering. Three-hour,
open-book exam; any non-communicating calculator permitted. Four questions constitute a complete
paper, each of equal value, and all four questions require calculation — the first four
problems as printed are worked below in full.
Reference texts: M.J. Moran, H.N. Shapiro, D.D. Boettner
& M.B. Bailey, Fundamentals of Engineering Thermodynamics, 8th ed. (ideal
vapor-compression refrigeration cycle, R-134a property tables); Y.A. Çengel & A.J.
Ghajar, Heat and Mass Transfer: Fundamentals and Applications, 5th ed. (convection
coefficients, forced-convection boundary layers); F.P. Incropera & D.P. DeWitt,
Fundamentals of Heat and Mass Transfer, 7th ed. (Blasius boundary-layer solution, Table
6.1); J.P. Holman, Heat Transfer, 10th ed. (radiation view factors for coaxial disks and
enclosures).
Problem 4: Radiation Exchange Between a Heater and a Conical Shield (25 points)
Given. Heater: flat black disk, diameter Dh = 10 cm
(r₁ = 0.05 m), temperature Th = 1200°C = 1473 K, sitting flush with the base
of the shield. Shield: black conical frustum (open top), base diameter 10 cm, top-opening
diameter Dtop = 20 cm (r₂ = 0.10 m), height L = 0.20 m, temperature
Ts = 100°C = 373 K.
Find. The net radiant heat transfer rate from the heater to the shield,
Qh→s.
Approach. The heater, the shield's lateral (frustum) surface and the open
top together form a 3-surface enclosure, with the open top standing in as a black,
non-reflecting fictitious surface facing the surroundings. Because the heater is flat it cannot
see itself ($F_{hh}=0$), so its view factor to the shield is $F_{h\to s}=1-F_{h\to top}$, where
$F_{h\to top}$ is the coaxial-parallel-disk view factor between the heater and an imaginary flat
disk covering the top opening (source's Configuration 3). With both surfaces black, the net
exchange follows directly from the two-black-surface relation.
Cross-section (schematic): a straight-up ray from the heater exits through
the open top without touching the shield; a shallower ray strikes the sloped shield wall.
View factor from the heater to the (fictitious) top-opening disk. Using the
source's Configuration 3 (coaxial parallel disks) with r₁ = 0.05 m, r₂ = 0.10 m,
h = 0.20 m: $R_1=r_1/h=0.25$, $R_2=r_2/h=0.5$,
$$X = 1+\frac{1+R_2^2}{R_1^2} = 1+\frac{1.25}{0.0625}=21$$
$$F_{h\to top} = \frac12\left[X-\sqrt{X^2-4(R_2/R_1)^2}\right]
= \frac12\left[21-\sqrt{441-16}\right] = \boxed{0.1922}$$
View factor from the heater to the shield. The heater is flat, so
$F_{hh}=0$ and, by the summation rule over the enclosure (heater, shield, top opening),
$$F_{h\to s} = 1 - F_{h\to top} = 1-0.1922 = \boxed{0.8078}$$
Net radiant heat transfer, heater to shield. With both surfaces black, the
direct two-surface exchange relation applies without any reflection correction; the heater's
area is $A_h=\pi r_1^2 = \pi(0.05)^2 = 7.854\times10^{-3}\ \text{m}^2$, so
$$Q_{h\to s} = A_h F_{h\to s}\,\sigma\left(T_h^4-T_s^4\right)$$
$$Q_{h\to s} = (7.854\times10^{-3})(0.8078)(5.67\times10^{-8})
\left(1473^4-373^4\right)$$
$$Q_{h\to s} = \boxed{1{,}690\ \text{W} \approx 1.69\ \text{kW}}$$