Fundamentals of Heat and Mass Transfer
Fundamentals of Heat and Mass Transfer
7th Edition
ISBN: 9780470501979
Author: Frank P. Incropera, David P. DeWitt, Theodore L. Bergman, Adrienne S. Lavine
Publisher: Wiley, John & Sons, Incorporated
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Chapter 12, Problem 12.128P

The oxidized-aluminum wing of an aircraft has a chord length of Lc ◰ 4 m and a spectral, hemispher- ical emissivity characterized by the following distribution.

Chapter 12, Problem 12.128P, The oxidized-aluminum wing of an aircraft has a chord length of Lc  4 m and a spectral, hemispher-

(a)Consider conditions for which the plane is on the ground where the air temperature is 27 C , the solar irradiation is 800 W/m 2 , and the effective sky temperature is 270 K. If the air is quiescent, what is the temperature of the top surface of the wing? The wing may be approximated as a horizontal, flat plate.

(b) When the aircraft is flying at an elevation of approximately 9000 m and a speed of 200 m/s, the air temperature, solar irradiation, and effective sky temperatureare 40 C , 1100  W/m 2  and 235K , respectively. What is the temperature of the wing’s top surface? The properties of the air may be approximated as ρ = 0.470  kg/m 3 ,   μ =1 .50x10 5 N s / m 2 , K = 0.021  W/m K, and Pr =0 .72 .

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Chapter 12 Solutions

Fundamentals of Heat and Mass Transfer

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