Steady State Conduction

Similar documents
Problem 1 Known: Dimensions and materials of the composition wall, 10 studs each with 2.5m high

Chapter 4. Unsteady State Conduction

CANKAYA UNIVERSITY FACULTY OF ENGINEERING MECHANICAL ENGINEERING DEPARTMENT ME 313 HEAT TRANSFER

Numerical Simulation of the Thermal Resposne Test Within the Comsol Multiphysics Environment

A) 0.77 N B) 0.24 N C) 0.63 N D) 0.31 N E) 0.86 N. v = ω k = 80 = 32 m/s. Ans: (32) 2 = 0.77 N

Surface and Contact Stress

NATURAL CONVECTION HEAT TRANSFER FROM A HEAT SINK WITH FINS OF DIFFERENT CONFIGURATION

Short notes for Heat transfer

Process Engineering Thermodynamics E (4 sp) Exam

Chapter 23 Electromagnetic Waves Lecture 14

OUTCOME 3 - TUTORIAL 1

Examiner: Dr. Mohamed Elsharnoby Time: 180 min. Attempt all the following questions Solve the following five questions, and assume any missing data

Phy 212: General Physics II 1 Chapter 18 Worksheet 3/20/2008

Physics 231 Lecture 31

EFFECTS OF WALL ORIENTATION AND THERMAL INSULATION ON TIME LAG AND DECREMENT FACTOR

rcrit (r C + t m ) 2 ] crit + t o crit The critical radius is evaluated at a given axial location z from the equation + (1 , and D = 4D = 555.

Thermal behavior of Surface Mount Device (SMD) for Spicer case

(1.1) V which contains charges. If a charge density ρ, is defined as the limit of the ratio of the charge contained. 0, and if a force density f

CHEM-443, Fall 2013, Section 010 Midterm 2 November 4, 2013

Study Group Report: Plate-fin Heat Exchangers: AEA Technology

Part One: Heat Changes and Thermochemistry. This aspect of Thermodynamics was dealt with in Chapter 6. (Review)

A Few Basic Facts About Isothermal Mass Transfer in a Binary Mixture

Materials Engineering 272-C Fall 2001, Lecture 7 & 8 Fundamentals of Diffusion

LECTURE 4 THE CONTENTS OF THIS LECTURE ARE AS FOLLOWS: 1.0 INTRODUCTION 2.0 SOURCES OF HEAT IN MINES 3.0 STRATA HEAT

Chapter 8 Reduction and oxidation

convection coefficient. The different property values of water at 20 C are given by: u W/m K, h=8062 W/m K

Chapter 5: Force and Motion I-a

Thermodynamics EAS 204 Spring 2004 Class Month Day Chapter Topic Reading Due 1 January 12 M Introduction 2 14 W Chapter 1 Concepts Chapter 1 19 M MLK

Lecture 12: Chemical reaction equilibria

( ) kt. Solution. From kinetic theory (visualized in Figure 1Q9-1), 1 2 rms = 2. = 1368 m/s

Outline. Steady Heat Transfer with Conduction and Convection. Review Steady, 1-D, Review Heat Generation. Review Heat Generation II

EHed of Curvature on the Temperature Profiles

EDA Engineering Design & Analysis Ltd

1. INTRODUCTION. In many polymer processing operations, molten polymers. emerge from dies into a stress field which deforms the

Design and Analysis of Gas Turbine Blade by Potential Flow Approach

Chapter 2 GAUSS LAW Recommended Problems:

Advanced Heat and Mass Transfer by Amir Faghri, Yuwen Zhang, and John R. Howell

Phys102 Final-061 Zero Version Coordinator: Nasser Wednesday, January 24, 2007 Page: 1

Instructions: Show all work for complete credit. Work in symbols first, plugging in numbers and performing calculations last. / 26.

Accelerated Chemistry POGIL: Half-life

Lecture 5: Equilibrium and Oscillations

AP CHEMISTRY CHAPTER 6 NOTES THERMOCHEMISTRY

CHAPTER 3 INEQUALITIES. Copyright -The Institute of Chartered Accountants of India

Introduction to Smith Charts

February 28, 2013 COMMENTS ON DIFFUSION, DIFFUSIVITY AND DERIVATION OF HYPERBOLIC EQUATIONS DESCRIBING THE DIFFUSION PHENOMENA

ES201 - Examination 2 Winter Adams and Richards NAME BOX NUMBER

CHAPTER 5. Solutions for Exercises

EE247B/ME218: Introduction to MEMS Design Lecture 7m1: Lithography, Etching, & Doping CTN 2/6/18

More Tutorial at

Phys102 First Major-122 Zero Version Coordinator: Sunaidi Wednesday, March 06, 2013 Page: 1

Pressure And Entropy Variations Across The Weak Shock Wave Due To Viscosity Effects

AC : USE OF SPREADSHEETS IN SOLVING HEAT CONDUCTION PROBLEMS IN FINS

THERMAL-VACUUM VERSUS THERMAL- ATMOSPHERIC TESTS OF ELECTRONIC ASSEMBLIES

Compressibility Effects

Equipment Fundamentals: Heat Exchangers. Chapter 3

Electric Current and Resistance

7-84. Chapter 7 External Forced Convection

Computational modeling techniques

Phys101 Final Code: 1 Term: 132 Wednesday, May 21, 2014 Page: 1

Fill in your name and ID No. in the space above. There should be 11 pages (including this page and the last page which is a formula page).

Chapter 39. A GUIDE TO THE DESIGN OP AIR BUBBLERS FOR MELTING ICE Simon Ince Hydraulics Section, National Research Council Ottawa, Canada

Methods of Determining Thermal Accommodation Coefficients from Free Molecular Flow Heat Transfer Data

WAVE RESISTANCE AND LIFT ON CYLINDERS BY A COUPLED ELEMENT TECHNIQUE. R. Eatock Taylor and G.X. Wu

4F-5 : Performance of an Ideal Gas Cycle 10 pts

Supporting information

The standards are taught in the following sequence.

Plan o o. I(t) Divide problem into sub-problems Modify schematic and coordinate system (if needed) Write general equations

Analytical investigations of thermo-geometrical parameters effects on heat transfer and performance of longitudinal radiating fin

Introduction to Three-phase Circuits. Balanced 3-phase systems Unbalanced 3-phase systems

Coupled Inductors and Transformers

Department of Civil Engineering & Applied Mechanics McGill University, Montreal, Quebec Canada

( ) ( ) ( ) ( ) ( z) ( )

Module 4: General Formulation of Electric Circuit Theory

Assume that the water in the nozzle is accelerated at a rate such that the frictional effect can be neglected.

Lecture 4. The First Law of Thermodynamics

Kinetics of Particles. Chapter 3

" 1 = # $H vap. Chapter 3 Problems

ANSWER KEY FOR MATH 10 SAMPLE EXAMINATION. Instructions: If asked to label the axes please use real world (contextual) labels

Unit 14 Thermochemistry Notes

Section 5.8 Notes Page Exponential Growth and Decay Models; Newton s Law

Chapter 2. Kinematics in One Dimension. Kinematics deals with the concepts that are needed to describe motion.

Effects of piezo-viscous dependency on squeeze film between circular plates: Couple Stress fluid model

Thermodynamics and Equilibrium

When a substance heats up (absorbs heat) it is an endothermic reaction with a (+)q

SUMMER REV: Half-Life DUE DATE: JULY 2 nd

Chapters 29 and 35 Thermochemistry and Chemical Thermodynamics

Session #22: Homework Solutions

Chapter 19. Electrochemistry. Dr. Al Saadi. Electrochemistry

Lifting a Lion: Using Proportions

Differentiation Applications 1: Related Rates

Use a lens holder fabricated from SiC. SiC has a larger CTE than C-C, i.e. it is better matched to the SFL6.

INVESTIGATION OF REVERSE ELECTRODIALYSIS UNITS BY MULTIPHYSICAL MODELLING

Lecture 13: Electrochemical Equilibria

Edexcel GCSE Physics

Chapter 17: Thermodynamics: Spontaneous and Nonspontaneous Reactions and Processes

Compressibility and collisional effects on thermal instability of a partially ionized medium

Engineering Approach to Modelling Metal THz Structures

WYSE Academic Challenge Regional Mathematics 2007 Solution Set

2015 Regional Physics Exam Solution Set

Computational modeling techniques

Transcription:

ECE309 Intrductin t Thermdynamics and Heat Transfer Spring 005 Tutrial # 7 Steady State Cnductin Prblem 1 Cnsider a naked persn standing in a rm at 0 C with an expsed surface area f 17m The deep bdy temperature f the human bdy is 37 C, and the thermal cnductivity f the human tissue near the skin is abut 03W/(m C) The bdy is lsing heat at a rate f 150W by natural cnvectin t the surrundings Taking the bdy temperature 05cm beneath the skin t be 37 C, determine the skin temperature f the persn and the cnvective heat transfer cefficient t the surrundings Slutin: Step 1: Draw a schematic diagram m Human Bdy T in T s T 0 cnd cnv Step : What t determine? The skin temperature f the persn, T s ; Cnvective heat transfer cefficient, h Step 3: The infrmatin given in the prblem statement Deep bdy temperature, T in 37 C, m temperature, T 0 0 C; Depth beneath the skin L05cm, Expsed surface Area, A17m ; Thermal cnductivity f the human tissue, k03w/(m C); Heat lss rate, 150 W Tutrial # 7 Page 1 f 5

ECE309 Intrductin t Thermdynamics and Heat Transfer Spring 005 Step 4: Assumptins Neglect the radiatin heat lss t the surrundings; The temperature wn t change with time(steady prblem) Step 5: Slve It s a ne-dimensin steady heat transfer prcess, and the cnductivity resistance is determined as L 05( cm) cnd 00098( C / W ) ka 03( W / m C) 17( m ) The heat lss is tatal cnd cnv 150 (W) The cnductive heat lss: cnd T cnd Tin Ts cnd Thus, Ts Tin cnd 37( C) 150( W ) 00098( C / W ) cnd The cnvective heat lss t the surrundings is calculated by cnv T cnv Ts T 1 ha S, the cnvective heat transfer cefficient, 0 355( C) h A( T s cnv T 0 ) 17( m 150( W ) ) # (355 0)( C) 569( W / m C) Step 6: Cnclusin statement The skin temperature f the persn will be 355 C and the cnvective heat transfer cefficient is 569 W/(m C) Tutrial # 7 Page f 5

ECE309 Intrductin t Thermdynamics and Heat Transfer Spring 005 Prblem As shwn in the figure, steam in a heating system flw thrugh ne side f rectangle plane (10cm*1cm) The plane is maintained at a temperature f 150 C ectangular aluminium ally 04-T6 s [k186 W/(m C)] with a cnstant width f 1cm and thickness f 01cm are attached t the plane The space between every tw adjacent s is 03cm The temperature f the surrunding air is 0 C and the cmbined cnvective heat transfer is 50W/(m C), Determine the verall effectiveness f the ned plane Slutin: Step 1: Draw a schematic diagram W1cm L1cm t01cm s03cm H10cm Step : What t determine? The verall effectiveness f the ned plane, Step 3: The infrmatin given in the prblem statement Tutrial # 7 Page 3 f 5

ECE309 Intrductin t Thermdynamics and Heat Transfer Spring 005 Plane surface temperature, T s 150 C, Atmsphere temperature, T 0 0 C; Plane gemetry: H10cm, and W1cm; Fin: cnductivity: k186 W/(m C), length: L1cm, thickness: t01cm, space: s03cm, width: W1cm The cmbined cnvective heat transfer: h50w/(m C) Step 4: Assumptins Neglect the radiatin heat lss t the surrundings; The temperature wn t change with time(steady prblem) Step 5: Slve CASE 1 With s n the plane: The efficiency f the s is determined frm Fig 8-59 t be t # ( L + ) h kt 0001 (001m + m) 50W / m C (186W / m C) (0001m) 016 which gives us the efficiency 095 the area f a is, t 0001 A W ( L + ) 01m (001m + m) 0005m S, the actual heat transfer rate thrugh the s is, # $ ha ( T s T0 ) 095 (50W / m # C) (0005m )(150 C 0 C) 15561W Fr the unned regin, the area is A un W s 01m 0003m 000036m S, the heat transfer rate thrugh an unned area is # un haun ( Ts T0 ) (50W / m # C) (000036m )(150 C 0 C) 34W the number f the s n the plane: H n t + s 10cm 01cm + 03cm 5 Tutrial # 7 Page 4 f 5

ECE309 Intrductin t Thermdynamics and Heat Transfer Spring 005 Fr the ttal heat transfer rate f the whle plane: ttal, n ( + un ) 5 (1561W + 34W ) 448 75W CASE N s n the plane The area f the whle plane is and the whle heat transfer rate is A n H W 01m 01m 001m n han ( Ts T0 ) (50W / m 78W # C) (001m )(150 C 0 C) The verall effectiveness f the ned plane ttal, n 44875W 78W 575 Step 6: Cnclusin statement The verall effectiveness f the ned plane is 575, which means the heat transfer rate is enhanced 575 times when attaching the s Tutrial # 7 Page 5 f 5