(a) Explanation Given: W = 200 m m = 0.2 m L = 12 m m = 0.012 m D = 100 m m = 0.1 m t = 1 m m = 0.001 m T 0 = 400 K T L = 350 K T ∞ = 300 K h = 150 W / m K 2 Assumptions: The steady state condition for the given heat rate. Heat conduction in fins is one dimensional. There is negligible radiation, uniform heat transfer with negligible variation in T ∞ The thermal conductivity of pure Aluminium at ( T 0 + T L 2 = 400 + 350 2 = 375 K ) is k = 240 W / m K Calculation: The temperature distribution in the fin is expressed by using the following general solution at distance ( x ) : θ ( x ) = T ( x ) − T ∞ θ ( x ) = C 1 e m x − C 2 e − m x … (1) The temperature distribution at boundary conditions is given by: At x = 0 , θ ( 0 ) = θ 0 θ 0 = T 0 − T ∞ θ 0 = C 1 + C 2 C 2 = θ 0 − C 1 … (2) And at x = L , θ ( L ) = θ L θ L = T L − T ∞ θ L = C 1 e m L + C 2 e − m L … (3) Put the value of C 2 by using eq. (2) in eq. (3): θ L = C 1 e m L + C 2 e − m L θ L = C 1 e m L + ( θ 0 − C 1 ) e − m L θ L = C 1 e m L + θ 0 e − m L − C 1 e − m L θ L = θ 0 e − m L + C 1 ( e m L − e − m L ) C 1 = θ L − θ 0 e − m L e m L − e − m L … (4) Now, put the value of ( C 1 = θ L − θ 0 e − m L e m L − e − m L ) in eq. (2): C 2 = θ 0 − θ L − θ 0 e − m L e m L − e − m L C 2 = θ 0 e m L − θ 0 e − m L − θ L + θ 0 e − m L e m L − e − m L C 2 = θ 0 e m L − θ L e m L − e − m L From eq. (1): θ ( x ) = C 1 e m x − C 2 e − m x θ ( x ) = ( θ L − θ 0 e − m L e m L − e − m L ) e m x − ( θ 0 e m L − θ L e m L − e − m L ) e − m x θ ( x ) = θ L e m x − θ 0 e − m L e m x − θ 0 e m L e − m x + θ L e − m x e m L − e − m L θ ( x ) = θ L e m x − θ 0 e m ( x − L ) + θ 0 e m ( L − x ) + θ L < (b) To determine The maximum power dissipation from top and the bottom plate

6th Edition

ISBN: 9780470501962

Author: Frank P. Incropera, David P. DeWitt, Theodore L. Bergman, Adrienne S. Lavine

Publisher: Wiley, John & Sons, Incorporated

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When energy travels from one object to another it is said to have undergone heat transfer. Heat transfer is nothing but the transfer of thermal energy or internal energy from one thing to another, like e.g., when a vessel with water, kept on top of a bur…

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Chapter 3, Problem 3.142P

(a)

To determine

The rate of fin heat transfer qf0 and qfL in terms of T0 and TL

(b)

To determine

The maximum power dissipation from top and the bottom plate

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Chapter 3, Problem 3.141P

Chapter 3, Problem 3.145P

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A differential element on the bracket is subjected to plane strain that has the following components:, Ɛx = 300 × 10-6, Ɛy = 150 × 10-6, Ɛxy = -750 x 10-6. Use the strain-transformation equations and determine the normal strain Ɛx in the X/ direction on an element oriented at an angle of 0 = 40°. Note, a positive angle, 0, is counter clockwise. x Enter your answer in micro strain to a precision of two decimal places. eg. if your answer is 300.15X106, please enter 300.15.

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Introduction to Heat Transfer

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The rate of fin heat transfer q f 0 and q f L in terms of T 0 and T L

Solution Summary: The author explains the steady state condition for the given heat rate.