ASSOCIATE DEGREE IN ENGINEERING EXAMINATIONS. SEMESTER 2 May 2013

Similar documents
PORTMORE COMMUNITY COLLEGE ASSOCIATE DEGREE IN ENGINEERING TECHNOLOGY

PORTMORE COMMUNITY COLLEGE

ASSOCIATE DEGREE IN ENGINEERING EXAMINATIONS SEMESTER /15 PAPER A

SECOND ENGINEER REG. III/2 APPLIED MECHANICS

MARKS DISTRIBUTION AS PER CHAPTER (QUESTION ASKED IN GTU EXAM) Name Of Chapter. Applications of. Friction. Centroid & Moment.

PDDC 1 st Semester Civil Engineering Department Assignments of Mechanics of Solids [ ] Introduction, Fundamentals of Statics

B.Tech. Civil (Construction Management) / B.Tech. Civil (Water Resources Engineering)

MANGA DISTRICT JOINT EVALUATION TEST 2010 Kenya Certificate of Secondary Education (K.C.S.E)

MAAE 2202 A. Come to the PASS workshop with your mock exam complete. During the workshop you can work with other students to review your work.

BE Semester- I ( ) Question Bank (MECHANICS OF SOLIDS)

ASSOCIATE DEGREE IN ENGINEERING EXAMINATIONS SEMESTER /13

ASSOCIATE DEGREE IN ENGINEERING TECHNOLOGY RESIT EXAMINATIONS. Semester 1 July 2012

Experiment: Torsion Test Expected Duration: 1.25 Hours

Physics P201 D. Baxter/R. Heinz. EXAM #3 November 21, :00 9:00 PM INSTRUCTIONS

Downloaded from Downloaded from / 1

Level 3 Cambridge Technical in Engineering

IDE 110 Mechanics of Materials Spring 2006 Final Examination FOR GRADING ONLY

SN QUESTION YEAR MARK 1. State and prove the relationship between shearing stress and rate of change of bending moment at a section in a loaded beam.

OUTCOME 1 - TUTORIAL 3 BENDING MOMENTS. You should judge your progress by completing the self assessment exercises. CONTENTS

2014 MECHANICS OF MATERIALS

MECHANICS OF MATERIALS. Prepared by Engr. John Paul Timola

[5] Stress and Strain

National Exams May 2015

Jordan University of Science & Technology PHYS 101A Final exam First semester 2007

A. Objective of the Course: Objectives of introducing this subject at second year level in civil branches are: 1. Introduction 02

3 Hours/100 Marks Seat No.

STRESS, STRAIN AND DEFORMATION OF SOLIDS

MECHANICS OF SOLIDS Credit Hours: 6


UNIVERSITY OF MANITOBA. All questions are of equal value. No marks are subtracted for wrong answers.

and F NAME: ME rd Sample Final Exam PROBLEM 1 (25 points) Prob. 1 questions are all or nothing. PROBLEM 1A. (5 points)

COURSE TITLE : APPLIED MECHANICS & STRENGTH OF MATERIALS COURSE CODE : 4017 COURSE CATEGORY : A PERIODS/WEEK : 6 PERIODS/ SEMESTER : 108 CREDITS : 5

QUESTION BANK SEMESTER: III SUBJECT NAME: MECHANICS OF SOLIDS

Physics 141 Rotational Motion 2 Page 1. Rotational Motion 2

ME 202 STRENGTH OF MATERIALS SPRING 2014 HOMEWORK 4 SOLUTIONS

BTECH MECHANICAL PRINCIPLES AND APPLICATIONS. Level 3 Unit 5

SECTION A. 8 kn/m. C 3 m 3m

Purpose of this Guide: To thoroughly prepare students for the exact types of problems that will be on Exam 3.

Determine the resultant internal loadings acting on the cross section at C of the beam shown in Fig. 1 4a.

Where, m = slope of line = constant c = Intercept on y axis = effort required to start the machine

Hours / 100 Marks Seat No.

CE 221: MECHANICS OF SOLIDS I CHAPTER 1: STRESS. Dr. Krisada Chaiyasarn Department of Civil Engineering, Faculty of Engineering Thammasat university

NAME: Given Formulae: Law of Cosines: Law of Sines:

Solid Mechanics Homework Answers

Honors Physics Review

Members Subjected to Torsional Loads

Overview. Dry Friction Wedges Flatbelts Screws Bearings Rolling Resistance

Experiment Two (2) Torsional testing of Circular Shafts

6. Find the net torque on the wheel in Figure about the axle through O if a = 10.0 cm and b = 25.0 cm.

Stress-Strain Behavior

The problem of transmitting a torque or rotary motion from one plane to another is frequently encountered in machine design.

7.6 Journal Bearings

Module 2 Stresses in machine elements. Version 2 ME, IIT Kharagpur

: APPLIED MECHANICS & STRENGTH OF MATERIALS COURSE CODE : 4021 COURSE CATEGORY : A PERIODS/ WEEK : 5 PERIODS/ SEMESTER : 75 CREDIT : 5 TIME SCHEDULE

ISHIK UNIVERSITY DEPARTMENT OF MECHATRONICS ENGINEERING

D : SOLID MECHANICS. Q. 1 Q. 9 carry one mark each.

Sample Question Paper

Matlab Sheet 2. Arrays

Sub. Code:

Mechanics of Materials

GATUNDU SOUTH KCSE REVISION MOCK EXAMS 2015

Sample Test Paper - I

QUESTION BANK DEPARTMENT: CIVIL SEMESTER: III SUBJECT CODE: CE2201 SUBJECT NAME: MECHANICS OF SOLIDS UNIT 1- STRESS AND STRAIN PART A

Chapter 3. Load and Stress Analysis. Lecture Slides

I B.TECH EXAMINATIONS, JUNE ENGINEERING MECHANICS (COMMON TO CE, ME, CHEM, MCT, MMT, AE, AME, MIE, MIM)

Mechanics of Solids. Mechanics Of Solids. Suraj kr. Ray Department of Civil Engineering

Please review the following statement: I certify that I have not given unauthorized aid nor have I received aid in the completion of this exam.

R13. II B. Tech I Semester Regular Examinations, Jan MECHANICS OF SOLIDS (Com. to ME, AME, AE, MTE) PART-A

Benha University College of Engineering at Benha Questions For Corrective Final Examination Subject: Fluid Mechanics M 201 May 24/ 2016

EDEXCEL NATIONAL CERTIFICATE/DIPLOMA FURTHER MECHANICAL PRINCIPLES AND APPLICATIONS UNIT 11 - NQF LEVEL 3 OUTCOME 4 - LIFTING MACHINES

Attempt ALL QUESTIONS IN SECTION A and ANY TWO QUESTIONS IN SECTION B Linear graph paper will be provided.

Static Failure (pg 206)

Samantha Ramirez, MSE. Stress. The intensity of the internal force acting on a specific plane (area) passing through a point. F 2

UNIT 4 FLYWHEEL 4.1 INTRODUCTION 4.2 DYNAMICALLY EQUIVALENT SYSTEM. Structure. Objectives. 4.1 Introduction

OUTCOME 1 MECHANICAL POWER TRANSMISSION SYSTEMS TUTORIAL 3 FLYWHEELS. On completion of this short tutorial you should be able to do the following.

CHAPTER 8: ROTATIONAL OF RIGID BODY PHYSICS. 1. Define Torque

PURE BENDING. If a simply supported beam carries two point loads of 10 kn as shown in the following figure, pure bending occurs at segment BC.

SRI CHANDRASEKHARENDRA SARASWATHI VISWA MAHAVIDHYALAYA

STRENGTH OF MATERIALS-I. Unit-1. Simple stresses and strains

KINGS COLLEGE OF ENGINEERING DEPARTMENT OF MECHANICAL ENGINEERING QUESTION BANK. Subject code/name: ME2254/STRENGTH OF MATERIALS Year/Sem:II / IV

UNIVERSITY OF BOLTON WESTERN INTERNATIONAL COLLEGE FZE BENG(HONS) MECHANICAL ENGINEERING SEMESTER TWO EXAMINATION 2016/2017 ENGINEERING PRINCIPLES 2

Stress Strain Elasticity Modulus Young s Modulus Shear Modulus Bulk Modulus. Case study

I certify that I have not given unauthorized aid nor have I received aid in the completion of this exam.

Bending Stress. Sign convention. Centroid of an area

SSC-JE MAINS ONLINE TEST SERIES / CIVIL ENGINEERING SOM + TOS

REVIEW. Final Exam. Final Exam Information. Final Exam Information. Strategy for Studying. Test taking strategy. Sign Convention Rules

Torsion Stresses in Tubes and Rods

N = Shear stress / Shear strain

Phys101 Third Major-161 Zero Version Coordinator: Dr. Ayman S. El-Said Monday, December 19, 2016 Page: 1

Sample 5. Determine the tension in the cable and the horizontal and vertical components of reaction at the pin A. Neglect the size of the pulley.

Hours / 100 Marks Seat No.

STATICS. Friction VECTOR MECHANICS FOR ENGINEERS: Eighth Edition CHAPTER. Ferdinand P. Beer E. Russell Johnston, Jr.

1 of 7. Law of Sines: Stress = E = G. Deformation due to Temperature: Δ

ME Final Exam. PROBLEM NO. 4 Part A (2 points max.) M (x) y. z (neutral axis) beam cross-sec+on. 20 kip ft. 0.2 ft. 10 ft. 0.1 ft.

ENGINEERING ENTRANCE EXAMINATION QUESTIONS IN MATHEMATICS NOTE: ANSWER ANY 11 QUESTIONS OUT OF 16 QUESTIONS

PHYSICS. Unit 3 Written examination Trial Examination SOLUTIONS

1. Attempt any ten of the following : 20

3.5 STRESS AND STRAIN IN PURE SHEAR. The next element is in a state of pure shear.

Final Examination Study Set 1. (Solutions will be in the Solutions Manual of Textbook)

Big Idea 4: Interactions between systems can result in changes in those systems. Essential Knowledge 4.D.1: Torque, angular velocity, angular

Transcription:

ASSOCIATE DEGREE IN ENGINEERING EXAMINATIONS SEMESTER 2 May 2013 COURSE NAME: CODE: Mechanical Engineering Science [8 CHARACTER COURSE CODE] GROUP: AD-ENG 1 DATE: TIME: DURATION: "[EXAM DATE]" "[TIME OF PAPER]" 2 hours INSTRUCTIONS: 1. This paper consists of SIX questions. 2. Candidates must attempt ANY FOUR questions on this paper. 3. All working MUST be CLEARLY shown. 4. Keep all parts of the same question together. 5. The use of non-programmable calculators is permitted. DO NOT TURN THIS PAGE UNTIL YOU ARE TOLD TO DO SO Instructions: Answer any FOUR (4) questions. 1

[Question 1] (a) A uniform beam AB has a length of 4.0 m and a mass of 30 kg. The beam rests on two supports at its ends. A 200 N load acts at a distance 1 m from end A and a 300 N load acts at a distance 1.5 m from end B. (i) Draw a free-body diagram showing all the forces acting on the beam. (ii) Determine the reactions at the supports A and B. [3 marks] [10 marks] (b) The diagram in Figure 1 shows a rectangular steel lamina of length 2.2 m and width 1.3 m. A square segment of side 0.6 m is removed from the lamina. y 2.2 m 0.6 m 0.6 m Figure 1 0.4 m 1.3 m x (i) Find the position of the centroid of the lamina from the y-axis. (ii) Find the mass of the weight of the lamina if its thickness is 0.8 cm. Density of steel = 7800 kg/m 3. [8 marks] [4 marks] [Question 2] (a) Define the terms: (i) mechanical advantage, (ii) velocity ratio, (iii) efficiency. [3 marks] (b) With the aid of a suitable labelled diagram, explain the operation of one (1) of the following simple machines. Screw jack, Differential wheel and axle 2

Wheel and axle Block and tackle pulley system [8 marks] (c) The table below gives values of load and effort from an experiment on a machine. Load W (kn) 1.0 2.0 3.0 4.0 5.0 6.0 Effort E (kn) 1.35 1.70 2.05 2.30 2.65 2.95 i. Use the data in the table above to draw an effort versus load graph. [6 marks] ii. State the law of the machine described by the data. [4 marks] iii. If the ideal mechanical advantage is 5. What is the effort required to overcome friction at a load of 4.5 kn? [4 marks] [Question 3] (a) Define the following: (b) (i) plane stress (ii) plane strain. [2 marks] (b) Sketch the stress-strain graph for a ferrous material and show the following points 1. the stress at the limit of proportionality ( lim ). 2. the ultimate tensile stress (UTS). 3. the yield stress ( yield ). [7 marks] (c) A steel reinforcing bar has a diameter of 32 mm and a gauge length of 6.0 m. Calculate tension in the bar if it extends by 0.5 mm. [8 marks] (d) (i) Define the terms: 1. shear stress, 2. shear strain. [2 marks] (ii) It is required to cut a cylindrical steel bar of diameter 32 mm using a shearing force of 300 kn. Determine the ultimate shear stress for the bar. [6 marks] 3

(Question 4) (a) Three point masses A, B and C of magnitudes 4 kg, 5 kg and 3 kg respectively are mounted on a shaft as shown in Figure 2. The distance of masses A, B and C, from the axis of the shaft are 10 cm, 15 cm and 20 cm respectively. If the shaft turns at 300 rev/min., determine B 5 kg 15 cm A 45 0 10 cm 4 kg 3 kg C 20 cm Figure 2 i. the magnitude and direction of the out of balance force. [11 marks] ii. the kinetic energy of the masses. [3 marks] (b) The speed of a rotating wheel decreases uniformly from 300 rev /min to rest in 10 seconds. Find: i. the angular deceleration of the wheel, [3 marks] ii. the number of revolution turned during the deceleration. [3 marks] (c) A spanner of length 35 cm was used to turn a bolt. A force of 140 N was applied perpendicular to the handle of the spanner. Find: i. the torque applied, [2 marks] ii. the work done if the spanner makes 6 revolutions. [3 marks] 4

(Question 5) (a) Explain the meaning of the following terms: (i) coefficient of limiting friction, (ii) angle of friction. [4 marks] (b) A 50 kg crate is pushed up an inclined plane at constant velocity by a 320 N force acting parallel to the plane. The angle of the inclined plane is 30 0, g = 9.80 m/s 2. (i) Draw a diagram and show all the forces acting on the crate. [3 marks] (ii) Determine: 1. the angle of friction. [2 marks] 2. the coefficient of friction between the crate and the inclined plane [4 marks] 3. the force acting parallel to the inclined plane which is required to make the crate slide down the plane with constant velocity. [4 marks] (c) Figure 3 shows how the torque acting on the shaft of a rotating machine varies over one complete revolution. Find the work done in one revolution. [8 marks] /(Nm) 150 100 (Question 6) 0 90 180 360 / 0 Figure 3 (a) (i) Differentiate between heat capacity and specific heat capacity. [2 marks] (ii) A piece of metal of mass 5.0 kg is heated to 200 0 C and immersed into 4.0 kg of water at 25 0 C contained in a brass container. The mass of the brass container is 20 kg. 5

Determine the final temperature of the system. [8 marks] Specific heat capacity of water = 4200 J/(kg K). Specific heat capacity of brass = 350 4200 J/(kg K). (b) (i) Distinguish between gauge pressure and absolute pressure. [2 marks] (ii) A U-tube water manometer is used to measure the pressure of a gas in a container. If the gauge pressure of the gas is 12 kn/m 2 and atmospheric pressure is 101.3 kn/m 2. 1. What is the absolute pressure of the gas in bars? [2 marks] 2. What will be the difference in the levels of the water in the two arms of the manometer? [5 marks] (c) A compressed air tank has a volume of 1.5 m 3. A pressure gauge fitted to this tank reads 1600 kn/m 2 when the barometric pressure was 1020 millibars. If the temperature of the air in the tank is 45 0 C, find the volume the air would occupy at s.t.p. Standard atmospheric pressure is 101.3 kn/m 2. [6 marks] ****END OF PAPER***** 6

ASSOCIATE DEGREE IN ENGINEERING SOLUTIONS SEMESTER 1 2009 DECEMBER COURSE NAME: CODE: Mechanical Engineering Sciencce [8 CHARACTER COURSE CODE] GROUP: "[AD-ENG 1 OR 2]" DATE: TIME: DURATION: "[EXAM DATE]" "[TIME OF PAPER]" 2 hr Solutions [Question 1] (a) (i) 200 N 300 N 300 N 1 m 1 m 0.75 m 1.25 m A R A 4.0 m B R B [3] (ii) M A = 0; - 200 x 1-300 x 2-300 x 2.75 + R B x 4 = 0-200 - 600-825 + R B x 4 = 0 7

(b) (i) 4 R B = 1625 R B = 406 N [5] M B = 0; 200 x 3 + 300 x 2 + 300 x 1.25 R A x 4 = 0 600 + 600 + 375 - R A x 4 = 0 4 R A = 1575 R A = 394 N [5] Check: F y = 0; 406 + 394-200 - 300-300 = 0 0 = 0 y 2.2 m A 0.6 m 0.6 m B 1.3 m 0.4 m x Consider the lamina is composed of a full rectangular lamina A and the cut-off part B of negative mass. A = 2.2 x 1.3 x A = 1.1 m = 2.86 m 2 B = - 0.6 x 0.6 x B = 2.2-0.4-0.3 = - 0.36 m 2 = 1.5 m [4] (A + B) x = A x A + B x B (2.86-0.36)x = 2.86 x 1.1-0.36 x 1.5 2.5 x = 3.146-0.54 = x = 1.04 m [4] (ii) V = A x w = 2.5 x 0.008 V = 0.02 m 3 m = V = 800 x 0.02 m = 16.0 kg [4] 8

[Question 2] (a) (i) Mechanical advantage is the ratio of load to effort for a machine. [1] (ii) Velocity ratio is the radio of the distance moved by the effort to the distance moved by the load. [1] (iii) Efficiency is the ratio of the work output to the work input. [1] (b) Labelled diagram and operation of a simple machine. [8] (c) (i) 3 Effort (kn) 2 1 0 0 1 2 3 4 5 6 4.5 kn Load(kN) [6] (ii) slope = (2.95-1.1)/(6-0) = 1.85/6 = 0.308 a = 0.308 b = 1.1 kn Law of the machine: E = 0.308 L + 1.1 kn [4] 9

(iii) From the graph, when the load is 4.5 kn the effort is 2.5 kn Ideal effort = 4.5/5 = 0.9 kn Friction effort = 2.5-0.9 = 1.6 kn [4] [Question 3] (a) (i) Plane stress is the ratio of the force per cross-sectional area of the material. [1] (ii) Plane strain is the ratio of the extension to the original length of the material. [1] (b) Stress UTS yield lim [7] Strain (c) A = π d 2 /4 = π (32) 2 /4 = 804 mm 2 A = 8.04 x 10-4 m 2 [2] L = 6.0 m e = 0.5 x 10-3 mm E = 2.03 x 10 11 Pa. E = F L/(A e) F = E A e/l [1] = (2.03 x 10 11 x 8.04 x 10-4 x 0.5 x 10-3 )/6 = (2.03 x 8.04 x 0.5 x 10 11 4-3 )/6 F = 13.6 x 10 3 N (13.6 kn) [5] (d) (i) 1. Shear stress is the ratio of the force to area, where the force acts parallel to the area. [1] 2. Shear strain is the ratio of the deformation of the material parallel to the force to the length perpendicular to the force. [1] (ii) A = 8.04 x 10-4 m 2 (from (c) above) Shear stress = force /area = 300 000 N/8.04 x 10-4 m 2 Shear stress = 37.3 x 10 7 N/m 2 [6] 10

(Question 4) (a) i. = 300 x 2 /60 = 10 rad/sec. [1] F = m 2 r F A = 4 x (10 ) 2 x 0.1 = 395 N F B = 5 x (10 ) 2 x 0.15 = 740 N F C = 3 x (10 ) 2 x 0.2 = 592 N [3] Determine the resultant of the three forces: x-component (N) y-component (N) F A 395 0 F B 0 740 F C 592 cos 225 0 = -418.6 592 sin 225 0 = -418.6 Total -23.6 321.4 [5] 321.4 N F R 23.6 N F R = (23.6 2 + 321.4 2 ) = 322 N [1] = tan -1 (321.4/23.6) = 86 0 [1] ii. K.E. = 0.5 m 2 r 2 = 0.5(10 ) 2 [ 4(0.1) 2 + 5(0.15) 2 + 3(0.2) 2 ] = 493.5[0.04 + 0.1125 + 0.12] K.E. = 134 J [3] 11

(b) i = 300 rpm = 10 rad/sec. f = 0 t = 10 s i. f = i + t 0 = 10 + 10 = - 10 /10 = - 3.14 rad/s 2 [3] ii. 2 2 f = i + 2 0 = (10 ) 2 + 2 x ( - 3.14) = 157 rad = 25 revs. [3] (c) i. = 140 x 0.35 = 49 N m [2] ii. W = = 49 x (6 x 2 ) W = 1847 J [3] (Question 5) (a) (i) The ratio of the limiting frictional force to the normal reaction for impending motion. [2] (ii) The angle between the reaction of the ground (frictional force plus normal reaction) and the normal reaction. [2] (b) (i) F k N 500 cos 30 0 30 0 500 sin 30 0 320 N [3] - (ii) 1. F y = 0; N - 500 cos 30 0 = 0 N = 433 N [3] F X = 0; 320-500 sin 30 0 - F k = 0 F k = 320-500 sin 30 0 = 70 N [3] 12

µ k = F k /N = 70/433 µ k = 0.16 [2] 2. = tan -1 (0.16) = 9.2 0 [2] 3. F k N 500 sin 30 0 30 0 P 500 cos 30 0 F X = 0; 500 sin 30 0 - F k - P = 0 250-70 - P = 0 P = 180 N (c) Find the work done in one revolution. [8] /(Nm) 150 100 0 90 180 360 / 0 Work done = area under graph = [100 x /2 + 0.5(100 + 150) x /2 + 0.5 x x 150] = [50 + 625 + 75] = (750) Work done = 2356 J [8] (Question 6) (a) (i) Heat capacity is the amount of heat absorbed or given off by a body when its temperature changes by one degree, whereas specific heat capacity is the 13

amount of heat given off or absorbed by 1 kg of a substance when the temperature changes by one degree, [2] (ii) Heat lost by hot metal ingot = heat absorbed by water + heat absorbed by brass container 5 x c ingot x (200-55) = 4 x 4200 x (55-25) + 10 x 350 (55-25) 725 x c ingot = 504 000 + 105 000 = 609 000 c ingot = 609 000/725 = 840 c ingot = 840 J/(kg K) [8] (b) (i) Gauge pressure is the excess pressure above atmospheric pressure and absolute pressure is the sum of the gauge pressure and atmospheric pressure. [2] (c) (ii) 1. absolute pressure = 12 + 200 = 212 kn/m 2. = 2.12 bars [2] 2. P = g h h = 12000/(1000 x 9.8) h = 1.22 m [5] A compressed air tank has a volume of 1.5 m 3. A pressure gauge fitted to this tank reads 1600 kn/m 2 when the barometric pressure was 1020 millibars. If the temperature of the air in the tank is 45 0 C, find the volume the air would occupy at s.t.p. Standard atmospheric pressure is 101.3 kn/m 2. P 1 = 1600 + 101.3 = 1701.3 kpa V 1 = 1.5 m 3 T 1 = 45 + 273 = 318 K P 2 = 101.3 kpa T 2 = 273 K [2] P 1 V 1 /T 1 = P 2 V 2 /T 2 V 2 = P 1 V 1 T 2 / P 2 T 1 = (1701.3) x 1.5 x 273/(101.3 x 318) V 2 = 21.6 m 3 [4] \ 14

Examination Paper Analysis Associate of Applied Science Degree Module: Mechanical Engineering Science Date: March 30, 2013 Examiner: Noel Brown Syllabus Objectives Question A B C D E F G H I J 1 X 2 X 3 X 4 X 5 X X 6 X X Question 1 Question is adequate for this level. Check editing. Question 2 Question is adequate for this level. Check Formatting. Question 3 Question is adequate for this level. B1 and B2 seems to be asking to identify the same point. Question 4 Question is adequate for this level. Question 5 Question is adequate for this level. Question 6 Question is adequate for this level. Check the solution 6b, it does not correspond to the question asked. Overall the paper provides good coverage of the syllabus objectives. Only a few changes are recommended, I have included some of the changes. Please ensure that the paper is proofread and all formatting are removed. Six questions are adequate for this exam, the time allotted (2 hours) is also adequate. The students should be able to complete four questions in 2 hours. 15