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To determine the effect of the temperature dependence of the thermal conductivity on the temperature distribution in a solid, consider a material for which this dependence may be represented as
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Chapter 2 Solutions
Fundamentals of Heat and Mass Transfer
- A 22-lb block B rests as shown on a 28-lb bracket A. The coefficients of friction are μs=0.30μs=0.30 and μk=0.25μk=0.25 between block B and bracket A, and there is no friction in the pulley or between the bracket and the horizontal surface. solved in a previous part. max weight of block C if block B is not to slide on bracket A is 5.045 lbs. Please solve for the acceleration of each Blockarrow_forwardTest 1 .DOCX * A File Edit View Tools Help INDUSTRIAL ENGINEERING PROGRAMME IMB 411-INDUSTRIAL LOGISTICS TEST 1- SEPTEMBER 12, 2012 Instructions: Answer all questions. Time allowed is 1.5 hours. Identify your script with your student number ONLY (Do not write your name). 1. Define the following terms (i) Logistics management (ii) Supply chain management (iii) Vertical integration in a supply chain (3 Marks) (3 Marks) (3 Marks) 2. (a) Using examples of your choice, briefly discuss the following levels of customer service (1) Pre-transaction elements (ii) Transaction elements (4 Marks) (4 Marks) (iii) Post-transaction elements (4 Marks) (b) "The challenge facing Dumelang Enterprise (Pty) Ltd is to establish the real profitability of their customers and to develop service strategies that will improve the profitability of all customers". As a logistics consultant, briefly discuss how you can advise Dumelang's customer service management. 3. (a) List the three main forms of inventory in a…arrow_forwardIt is decided to install several single-jet Pelton wheels to produce a total power of 18 MW. The available head is 246 m. The wheel rotational speed is 650 rpm and the speed ratio (❤) = 0.46. The diameter of the nozzle (jet) is limited to be 0.167 m with a Cv of 0.95. The efficiency of each turbine is 87%. Determine: (1) The number of Pelton wheels to be used, and (2) The bucket angle.arrow_forward
- (I) [40 Points] Using centered finite difference approximations as done in class, solve the equation for O: d20 dx² + 0.010+ Q=0 subject to the boundary conditions shown in the stencil below. Do this for two values of Q: (a) Q = 0.3, and (b) Q= √(0.5 + 2x)e-sinx (cos(5x)+x-0.5√1.006-x| + e −43*|1+.001+x* | * sin (1.5 − x) + (cosx+0.001 + ex-1250+ sin (1-0.9x)|) * x - 4.68x4. For Case (a) (that is, Q = 0.3), use the stencil in Fig. 1. For Case (b), calculate with both the stencils in Fig. 1 and Fig 2. For all the three cases, show a table as well as a plot of O versus x. Discuss your results. Use MATLAB and hand in the MATLAB codes. 1 0=0 x=0 2 3 4 0=1 x=1 Fig 1 1 2 3 4 5 6 7 8 9 10 11 0=0 x=0 0=1 x=1 Fig 2arrow_forwardFig 2 (II) [60 Points] Using centered finite difference approximation as done in class, solve the equation: 020 020 + მx2 მy2 +0.0150+Q=0 subject to the boundary conditions shown in the stencils below. Do this for two values of Q: (a) Q = 0.3, and (b) Q = 10.5x² + 1.26 * 1.5 x 0.002 0.008. For Case (a) (that is, Q = 0.3) use Fig 3. For Case (b), use both Fig. 3 and Fig 4. For all the three cases, show a table as well as the contour plots of versus (x, y), and the (x, y) heat flux values at all the nodes on the boundaries x = 1 and y = 1. Discuss your results. Use MATLAB and hand in the MATLAB codes. (Note that the domain is (x, y)e[0,1] x [0,1].) 0=0 0=0 4 8 12 16 10 Ꮎ0 15 25 9 14 19 24 3 11 15 0=0 8-0 0=0 3 8 13 18 23 2 6 сл 5 0=0 10 14 6 12 17 22 1 6 11 16 21 13 e=0 Fig 3 Fig 4 Textbook: Numerical Methods for Engineers, Steven C. Chapra and Raymond P. Canale, McGraw-Hill, Eighth Edition (2021).arrow_forwardShip construction question. Sketch and describe the forward arrangements of a ship. Include componets of the structure and a explanation of each part/ term. Ive attached a general fore end arrangement. Simplfy construction and give a brief describion of the terms.arrow_forward
- Problem 1 Consider R has a functional relationship with variables in the form R = K xq xx using show that n ✓ - (OR 1.) = i=1 2 Их Ux2 Ихэ 2 (177)² = ² (1)² + b² (12)² + c² (1)² 2 UR R x2 x3arrow_forward4. Figure 3 shows a crank loaded by a force F = 1000 N and Mx = 40 Nm. a. Draw a free-body diagram of arm 2 showing the values of all forces, moments, and torques that act due to force F. Label the directions of the coordinate axes on this diagram. b. Draw a free-body diagram of arm 2 showing the values of all forces, moments, and torques that act due to moment Mr. Label the directions of the coordinate axes on this diagram. Draw a free body diagram of the wall plane showing all the forces, torques, and moments acting there. d. Locate a stress element on the top surface of the shaft at A and calculate all the stress components that act upon this element. e. Determine the principal stresses and maximum shear stresses at this point at A.arrow_forward3. Given a heat treated 6061 aluminum, solid, elliptical column with 200 mm length, 200 N concentric load, and a safety factor of 1.2, design a suitable column if its boundary conditions are fixed-free and the ratio of major to minor axis is 2.5:1. (Use AISC recommended values and round the ellipse dimensions so that both axes are whole millimeters in the correct 2.5:1 ratio.)arrow_forward
- Principles of Heat Transfer (Activate Learning wi...Mechanical EngineeringISBN:9781305387102Author:Kreith, Frank; Manglik, Raj M.Publisher:Cengage Learning
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