ASSOCIATE DEGREE IN ENGINEERING EXAMINATIONS SEMESTER /15 PAPER A

Similar documents
ASSOCIATE DEGREE IN ENGINEERING EXAMINATIONS SEMESTER /13

ASSOCIATE DEGREE IN ENGINEERING EXAMINATIONS. SEMESTER 2 May 2013

PORTMORE COMMUNITY COLLEGE ASSOCIATE DEGREE IN ENGINEERING TECHNOLOGY

PORTMORE COMMUNITY COLLEGE

Check Homework. Reading Quiz Applications Equations of Equilibrium Example Problems Concept Questions Group Problem Solving Attention Quiz

CHAPTER 2: EQUILIBRIUM OF RIGID BODIES

Statics Chapter II Fall 2018 Exercises Corresponding to Sections 2.1, 2.2, and 2.3

Engineering Mechanics: Statics in SI Units, 12e

EQUATIONS OF EQUILIBRIUM & TWO- AND THREE-FORCE MEMEBERS

EQUATIONS OF EQUILIBRIUM & TWO- AND THREE-FORCE MEMEBERS

== Delft University of Technology == Give on the upper right. Exam STATICS /

Chapter 2. Shear Force and Bending Moment. After successfully completing this chapter the students should be able to:

Module 6. Approximate Methods for Indeterminate Structural Analysis. Version 2 CE IIT, Kharagpur

RIN: Monday, May 16, Problem Points Score Total 100

8.3 Shear and Bending-Moment Diagrams Constructed by Areas

BTECH MECHANICAL PRINCIPLES AND APPLICATIONS. Level 3 Unit 5

Solution ME 323 EXAM #2 FALL SEMESTER :00 PM 9:30 PM Nov. 2, 2010

Ishik University / Sulaimani Architecture Department. Structure. ARCH 214 Chapter -5- Equilibrium of a Rigid Body

8.1 Internal Forces in Structural Members

1. The horizontal beam represented in Examination Figure 6 carries three loads P 1. and R 2

ARCH 631 Note Set 2.1 F2010abn. Statics Primer

INTI INTERNATIONAL UNIVERSITY FOUNDATION PROGRAMME (ENGINEERING/SCIENCE) (CFSI) EGR 1203: ENGINEERING MECHANICS FINAL EXAMINATION: AUGUST 2015 SESSION

Delft Applied Mechanics Course: Statics AE1-914-I. 18 August 2004, 9:00 12:00

M D P L sin x FN L sin C W L sin C fl cos D 0.

Shear Force and Bending Moment Diagrams for a Beam Steven Vukazich San Jose State University

ENGR-1100 Introduction to Engineering Analysis. Lecture 13

STATICS. FE Review. Statics, Fourteenth Edition R.C. Hibbeler. Copyright 2016 by Pearson Education, Inc. All rights reserved.

7 STATICALLY DETERMINATE PLANE TRUSSES

Engineering Mechanics Statics

Eng Sample Test 4

SLOPE-DEFLECTION METHOD

F R. + F 3x. + F 2y. = (F 1x. j + F 3x. i + F 2y. i F 3y. i + F 1y. j F 2x. ) i + (F 1y. ) j. F 2x. F 3y. = (F ) i + (F ) j. ) j

MECHANICS OF MATERIALS

Chapter Objectives. Copyright 2011 Pearson Education South Asia Pte Ltd

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

Types of Structures & Loads

MOMENT OF A COUPLE. Today s Objectives: Students will be able to. a) define a couple, and, b) determine the moment of a couple.

SOLUTION 8 1. a+ M B = 0; N A = 0. N A = kn = 16.5 kn. Ans. + c F y = 0; N B = 0

TUTORIAL SHEET 1. magnitude of P and the values of ø and θ. Ans: ø =74 0 and θ= 53 0

EQUATIONS OF MOTION: RECTANGULAR COORDINATES

Internal Internal Forces Forces

Chapter 04 Equilibrium of Rigid Bodies

P.E. Civil Exam Review:

Module 3. Analysis of Statically Indeterminate Structures by the Displacement Method

Mechanics of Materials

Easy. P5.3 For equilibrium: f = F and n = F g. Also, f = n, i.e., f n F F g. (a) 75.0 N N N N (b) ma y.

3.1 CONDITIONS FOR RIGID-BODY EQUILIBRIUM

Module 2. Analysis of Statically Indeterminate Structures by the Matrix Force Method

EQUILIBRIUM OF RIGID BODIES

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

However, the friction forces are limited in magnitude and will not prevent motion if sufficiently large forces are applied.

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

APPLIED MECHANICS I Resultant of Concurrent Forces Consider a body acted upon by co-planar forces as shown in Fig 1.1(a).

EGN 3310 Practice Final Spring 2017

Announcements. Equilibrium of a Particle in 2-D


Physics B Newton s Laws AP Review Packet

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

Announcements. Equilibrium of a Rigid Body

where x and y are any two non-parallel directions in the xy-plane. iii) One force equation and one moment equation.

two structural analysis (statics & mechanics) Structural Requirements Structure Requirements Structure Requirements serviceability efficiency

Module 2. Analysis of Statically Indeterminate Structures by the Matrix Force Method

Beams. Beams are structural members that offer resistance to bending due to applied load

S in. S in 40 M s = (20.35)(30.0) M s = 611 in-lb clockwise = 2.12 m with a negative action. The moment about B is

Chapter 5 Equilibrium of a Rigid Body Objectives

5. Plane Kinetics of Rigid Bodies

E 490 FE Exam Prep. Engineering Mechanics

Supplement: Statically Indeterminate Frames

Chapter Objectives. Copyright 2011 Pearson Education South Asia Pte Ltd

Bending Stress. Sign convention. Centroid of an area

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

ENG202 Statics Lecture 16, Section 7.1

Chapter 5. The Laws of Motion

ES226 (01) Engineering Mechanics: Statics Spring 2018 Lafayette College Engineering Division

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

CHAPTER 6: Shearing Stresses in Beams

if the initial displacement and velocities are zero each. [ ] PART-B

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

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

EQUATIONS OF EQUILIBRIUM & TWO- AND THREE-FORCE MEMBERS

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.

EMA 3702 Mechanics & Materials Science (Mechanics of Materials) Chapter 4 Pure Bending

PROBLEMS ON EQUILIBRIUM OF PARTICLES

Chapter 4.1: Shear and Moment Diagram

Name. ME 270 Fall 2005 Final Exam PROBLEM NO. 1. Given: A distributed load is applied to the top link which is, in turn, supported by link AC.

3.032 Problem Set 1 Fall 2007 Due: Start of Lecture,

Module 3. Analysis of Statically Indeterminate Structures by the Displacement Method

PHYS 111 K SECOND HOUR EXAM 2015

Chapter 9- Static Equilibrium

Equilibrium of Rigid Bodies

EQUATIONS OF EQUILIBRIUM & TWO- AND THREE-FORCE MEMBERS

PROBLEMS. m s TAC. m = 60 kg/m, determine the tension in the two supporting cables and the reaction at D.

5.2 Rigid Bodies and Two-Dimensional Force Systems

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

Stress Analysis Lecture 4 ME 276 Spring Dr./ Ahmed Mohamed Nagib Elmekawy

UNIT II 1. Sketch qualitatively the influence line for shear at D for the beam [M/J-15]

7.6 Journal Bearings

3D Force Couple System and Resultant. Q.No.1: Replace the force system by an equivalent force and couple moment at point A.

0.3 m. 0.4 m. 0.3 m. A 2 kn. 0.4 m. tan γ = 7. (BC = kn) γ = Fx = BC cos θ + AC cos γ =0

Chapter 5. The Laws of Motion

Transcription:

SSOCITE DEGREE IN ENGINEERING EXMINTIONS SEMESTER 2 2014/15 PPER COURSE NME: ENGINEERING MECHNICS - STTICS CODE: ENG 2008 GROUP: D ENG II DTE: May 2015 TIME: DURTION: 2 HOURS INSTRUCTIONS: 1. This paper consists of SIX questions. 2. Candidates must attempt NY FOUR questions on this paper. 3. ll working MUST be CLERLY shown. 4. Keep all parts of the same question together. 5. The use of programmable calculators is permitted. DO NOT TURN THIS PGE UNTIL YOU RE TOLD TO DO SO

[Question 1] (a) Figure 1.1 below shows four forces acting on a particle at the origin. Determine the magnitude of P and the orientation of the 800 N force so that the particle is in equilibrium. [10 marks] 800 N y 700 N 60 0 P Figure 1.1 300 N (b) Epress the force F in Figure 1.2 in Cartesian vector form. [7 marks] z 50 0 60 0 F y 100 N Figure 1.2 (c) Determine the moment of the couple formed by the two forces F and F acting on the bar B. z [8 marks] F = {-6 i + 3 j + 3k } N -F = {6 i - 3 j - 3k } N B y Figure 1.3

[Total = 25 Marks] [Question 2] (a) The loading on the beam B in Figure 2.1 consists of three point loads and a couple moment. Replace the loading on the beam by a single resultant force. Specify where the force acts measured from. [15 marks] 450 N 300 N 700 N 60 0 B 60 0 2 m 4 m 3 m 1500 Nm Figure 2.1 (b) Find the magnitude of the projected component of the force F along the cable C in Figure 2.2. [10 marks] z C 4 m 2 m B 6 m F = 500 N y 4 m Figure 2.2 [Total = 25 marks]

[Question 3] (a) girder B shown in Figure 3.1 has four concentrated loads acting on it. 7 kn 7 kn 7 kn 7 kn 2 m 2 m 2 m 2 m 1 m B Figure 3.1 Neglecting the weight of the girder, determine: (i) the reactions at and B. [5 marks] (ii) Draw the shear force diagram. [8 marks] (iii) Draw the bending moment diagram. Indicate the maimum value of the bending moment. [12 marks] [Total = 25 marks] [Question 4] Figure 4.1 shows a plane frame which is simply supported. 12 kn 6 kn 6 kn H G F E 2 m B C D 2 m 2m 2m Figure 4.1 (a) Determine the reactions at and D. [6 marks] (b) Identify the zero-force member(s) and justify your answer. [3 marks] (c) Using the method of sections determine the forces in the members BC, GC and GF. [16 marks]

[Total = 25 marks] 5. (a) uniform crate has a mass of 40 kg and rests on a floor for which s = 0.25. The crate is pushed with a force F at an angle of 30 0 above the horizontal as shown in Figure 5.1. F 30 0 crate Figure 5.1 floor Determine the smallest force F required to move the crate. [13 marks] (b) crate of weight 200 lb is supported by a cord which wraps over a pipe as shown in Figure 5.2. F 200 lb Figure 5.2 (i) Determine the minimum force F which is required to prevent the crate from slipping downwards if the cord passes once over the pipe ( = 180 0 ). [8 marks]

(ii) What tension is required to allow the crate to move downwards at constant velocity when = 180 0. [4 marks] s = 0.25 and k = 0.2. [Total = 25 marks] [Question 6] (a) Eplain the meaning of the term moment of inertia. [2 marks] (b) With the aid of a diagram eplain the parallel ais theorem. [4 marks] (c) The cross-section of a beam is shown in Figure 6.1. y 120 mm 20 mm 50 mm 125 mm 20 mm Figure 6.1 (i) Determine the location of the centroid of the beam from the -ais. [8 marks] (ii) Compute the moment of inertia of the area about the -ais. [11 marks]

[Total = 25 marks] END OF EXM SSOCITE DEGREE IN ENGINEERING SOLUTIONS SEMESTER 2 2015 MY COURSE NME: ENGINEERING STTICS CODE: GROUP: D-ENG 2 DTE: MY 2015 TIME: DURTION: 2 HOURS SOLUTIONS: 1. (a) F = 0; 700 cos 60 0 + 300-800 cos = 0... (1) [2] F y = 0; 700 sin 60 0 + 800 sin - P = 0...(2) [2] From (1): 800 cos = 700 cos 60 0 + 300 = 650 cos = 650/800 = 0.8125 = cos -1 (0.8125) = 35.7 0 [3] Substituting into ((2):

P = 700 sin 60 0 + 800 sin = 700 sin 60 0 + 800 sin 35.7 0 P = 606 + 487 = 1093 N [3] (b) F = 100 N F cos 40 0 = F = 100 F = 100/cos40 0 = 131 N [2] F = 100 cos 60 0 = 50 N [1] F y = 100 cos 30 0 = 86.6 N [1] F z = 131 cos 50 0 = 84.2 N [2] F = { 50 i + 86.6 j + 84.2 k} N [1] (c) M = r F = (0.6 k + 0.8 j) (- 6 i + 3 j + 3 k) = [3] i j k 0 0.8 0.6 [1] - 6 3 3 = i 0.8-0.6 - j 0-0.6 + k 0 0.8 3 3-6 3-6 3 [2] = i ( 2.4 + 1.8 ) - j (0-3.6) + k (0 + 4.8) M = {4.2 i + 3.6 j + 4.8 k} Nm [2] 2. (a) 450 N 300 N 700 N 60 0 B 60 0 2 m 4 m 3 m 1500 Nm F = 450 cos 60 0-700 cos 60 0 = 225-350 = -125 N [3] F y = -450 sin 60 0-300 - 700 sin 60 0 125 N = -389.7-300 - 606.2 1296 N F = -1296 N R [3] F R = [(-125 2 ) + (-1296) 2 ] = 1302 N

= tan -1 (1296/125) = 84.5 0 [2] M = - 450 2 sin 60 0-300 6-700 9 sin 60 0-1500 = - 779-1800 - 5456-1500 M = -9535 Nm [3] d 84.5 0 1302 N M = -9535 1302 d sin 84.5 0 = 9535 d = 9535/(1302 sin 84.5 0 ) d = 7.36 m [4] (b) C 2 m B F = 500 N 4 m 6 m 4 m r B = {- 6 i + 2 k} m [1] r C = {- 4 j + 4 k} m [1] u B = (- 6 i + 2 k)/ (6 2 + 2 2 ) = (- 6 i + 2 k)/6.32 [2] u C = (- 4 j + 4 k)/ (4 2 + 4 2 ) = (- 4 j + 4 k)/5.66 [2] F = (500) (- 6 i + 2 k)/6.32 [1] The projected component of F along C is given by F. u C.

F. u C = (500/6.23) (- 6 i + 2 k).(- 4 j + 4 k)/5.66 = 14.18 8 = 113 N [3] 3. 7 kn 7 kn 7 kn 7 kn 2 m 2 m 2 m 2 m 1 m B (a) M = 0; - 7 2-7 4-7 6-7 8 + R B 9 = 0-14 - 28-42 - 56 + 9 R B = 0-140 + 9 R B = 0 R B = 140/9 = 15.6 kn M B = 0; -R 9 + 7 1 + 7 3 + 7 5 + 7 7 = 0-9 R + 7 + 21 + 35 + 49 = 0 R = 112/9 = 12.4 kn [5] (b)

7 kn 7 kn 7 kn 7 kn 2 m 2 m 2 m 2 m 1 m B V(kN) 12.4 kn 24.8 knm 5.4 kn 10.8 knm -1.6 kn -8.6 kn -3.2 knm -17.2 knm -15.6 knm -15.6 kn M(kNm) 24.8 knm 15.2 knm 35.6 knm 32.4 knm

M ma = 35.6 knm 4. (a) R 12 kn 6 kn 6 kn 2 m 2 m 2m D R D M = 0; -12 2-6 4-6 6 + R B 6 = 0-24 - 24-36 + 6 R B = 0 R B = 84/6 = 14 kn [3] M D = 0; -R 6 + 6 2 + 12 4 = 0 6 R = 12 + 48 = 60 R = 60/6 = 10 kn [3] (b) Zero force members are : B and FE. [3 ] (c) 12 kn H G 45 0 F GF 2 m F GC 10 kn 2 m B F BC [4] Using the section shown above:

F y = 0; 10-12 - F GC sin 45 0 = 0 F GC = (10-12)/ sin 45 0 = - 2.83 kn (S) [4] M G = 0; F BC 2-10 2 = 0 F BC = 20/2 = 10 kn (T) [4] F = 0; F GF + F BC + F GC cos45 0 = 0 F GF + 10 + (-2.83) cos45 0 = 0 F GF = -10 + 2.83 cos45 0 = -8.0 kn (S) [4] 5. (a) F 30 0 crate [3] f floor N mg Equation of equilibrium: F = 0; F cos 30 0 - N = 0 F cos 30 0-0.25 N = 0.....(1) [3] F y = 0; -Fsin 30 0-40 g + N = 0... (2) [2] From (1): N = Fcos 30 0 /0.25.... (3) Substituting equation (3) into (2) gives: -Fsin 30 0-40(9.8) + Fcos 30 0 /0.25 = 0-0.5 F - 392 + 3.46 F = 0 or 2.96 F = 392 F = 132 N [5] (b) (i) T 2 = 200 lb = and = 0.25

T 2 = T 1 e 200 = T 1 ep( 0.25 ) T 1 = 200/ ep( 0.25 ) T 1 = 91.2 lb [6] (ii) T 1 = 200/ ep( 0.2 ) = 107 lb [3] 6. (a) Moment of inertia is the second moment of area of a cross-section about a given ais. [2] (b) rea = G d Consider the figure shown above with and centroid at point G. The centroidal ais is -. The moment of inertia about the centroidal ais is I. The moment of inertia about the new ais - which is at a perpendicular distance d from the centroidal ais is given by I = I + d 2 [4] (c) y 120 mm 2 20 mm 50 mm 1 125 mm

Divide the cross-section in parts 1 and 2 as shown in the diagram: (i) 1 = 125 20 = 2500 mm 2 ; y 1 = 125/2 = 62.5 mm [2] 2 = 120 20 = 2400 mm 2 ; y 1 = 125 + 20/2 = 135 mm [2] ( 1 + 2 ) ŷ = 1 y 1 + 2 y 2 (2500 + 2400) ŷ = 2500 62.5 + 2400 135 [2] 4900 ŷ = 156250 + 324000 = 480250 ŷ = 480250/4900 = 98.01 mm [2] (ii) I 1 = (1/12) 20 125 3 + 2500 (125/2) 2 = 3.255 10 6 + 9.766 10 6 I 1 = 13.02 10 6 mm 4 [5] I 2 = (1/12) 120 20 3 + 2400 (135) 2 = 0.8 10 6 + 43.74 10 6 I 2 = 44.54 10 6 mm 4 [5] I = I 1 + I 2 = (13.02 + 44.54) 10 6 mm 4 I = 57.56 10 6 mm 4 [1]

Eamination Paper nalysis ssociate of pplied Science Degree Module: Engineering Mechanics (Statics) Eaminer: Noel Brown pril 2, 2015 Syllabus Objectives Question B C D E F G H I J 1 X X X 2 X X 3 X X 4 X 5 X 6 X Question 1 Question is adequate for this level. Question 2 Question is adequate for this level. Question 3 Question is adequate for this level. Question 4 Question is adequate for this level. Question 5 Question is adequate for this level. Question 6 Question is adequate for this level.

The paper need to be formatted properly. I have included some of the formatting. Please ensure that the paper is proofread before it is sent to the second eaminer. Overall both papers are provides good coverage of the syllabus objectives. The time allotted is also adequate for the student to safely complete four questions. ny of the papers could be used as the final.