Exam CT3109 STRUCTURAL MECHANICS april 2011, 09:00 12:00 hours

Similar documents
V. DEMENKO MECHANICS OF MATERIALS LECTURE 6 Plane Bending Deformation. Diagrams of Internal Forces (Continued)

Module 1. Energy Methods in Structural Analysis

1 Bending of a beam with a rectangular section

Module 2. Analysis of Statically Indeterminate Structures by the Matrix Force Method. Version 2 CE IIT, Kharagpur

MECHANICS OF MATERIALS

Chapter 5 Bending Moments and Shear Force Diagrams for Beams

ES.182A Topic 32 Notes Jeremy Orloff

Shear and torsion interaction of hollow core slabs

Explain shortly the meaning of the following eight words in relation to shells structures.

BME 207 Introduction to Biomechanics Spring 2018

Lecture 13 - Linking E, ϕ, and ρ

Statically indeterminate examples - axial loaded members, rod in torsion, members in bending

13.4 Work done by Constant Forces

Physics 121 Sample Common Exam 1 NOTE: ANSWERS ARE ON PAGE 8. Instructions:

Plates on elastic foundation

6.5 Plate Problems in Rectangular Coordinates

Plate Theory. Section 11: PLATE BENDING ELEMENTS

KEY CONCEPTS. satisfies the differential equation da. = 0. Note : If F (x) is any integral of f (x) then, x a

Advanced Computational Analysis

Kirchhoff and Mindlin Plates

Plate Theory. Section 13: PLATE BENDING ELEMENTS

7.3 Problem 7.3. ~B(~x) = ~ k ~ E(~x)=! but we also have a reected wave. ~E(~x) = ~ E 2 e i~ k 2 ~x i!t. ~B R (~x) = ~ k R ~ E R (~x)=!

Families of Solutions to Bernoulli ODEs

Mathematics Extension Two

Year 12 Mathematics Extension 2 HSC Trial Examination 2014

Candidates must show on each answer book the type of calculator used.

ragsdale (zdr82) HW2 ditmire (58335) 1

2A1A Vector Algebra and Calculus I

Solution Manual. for. Fracture Mechanics. C.T. Sun and Z.-H. Jin

Sample Exam 5 - Skip Problems 1-3

ME 141. Lecture 10: Kinetics of particles: Newton s 2 nd Law

KINEMATICS OF RIGID BODIES

DETERMINATION OF MECHANICAL PROPERTIES OF NANOSTRUCTURES WITH COMPLEX CRYSTAL LATTICE USING MOMENT INTERACTION AT MICROSCALE

Higher Checklist (Unit 3) Higher Checklist (Unit 3) Vectors

6.2 CONCEPTS FOR ADVANCED MATHEMATICS, C2 (4752) AS

x 2 1 dx x 3 dx = ln(x) + 2e u du = 2e u + C = 2e x + C 2x dx = arcsin x + 1 x 1 x du = 2 u + C (t + 2) 50 dt x 2 4 dx

2/20/ :21 AM. Chapter 11. Kinematics of Particles. Mohammad Suliman Abuhaiba,Ph.D., P.E.

Session Trimester 2. Module Code: MATH08001 MATHEMATICS FOR DESIGN

TO: Next Year s AP Calculus Students

99/105 Comparison of OrcaFlex with standard theoretical results

Machine Design II Prof. K.Gopinath & Prof. M.M.Mayuram. Drum Brakes. Among the various types of devices to be studied, based on their practical use,

20 MATHEMATICS POLYNOMIALS

2/2/ :36 AM. Chapter 11. Kinematics of Particles. Mohammad Suliman Abuhaiba,Ph.D., P.E.

A. Limits - L Hopital s Rule. x c. x c. f x. g x. x c 0 6 = 1 6. D. -1 E. nonexistent. ln ( x 1 ) 1 x 2 1. ( x 2 1) 2. 2x x 1.

13: Diffusion in 2 Energy Groups

A little harder example. A block sits at rest on a flat surface. The block is held down by its weight. What is the interaction pair for the weight?

In-Class Problems 2 and 3: Projectile Motion Solutions. In-Class Problem 2: Throwing a Stone Down a Hill

The Wave Equation I. MA 436 Kurt Bryan

a 2 +x 2 x a 2 -x 2 Figure 1: Triangles for Trigonometric Substitution

200 points 5 Problems on 4 Pages and 20 Multiple Choice/Short Answer Questions on 5 pages 1 hour, 48 minutes

Warm-up for Honors Calculus

1/31/ :33 PM. Chapter 11. Kinematics of Particles. Mohammad Suliman Abuhaiba,Ph.D., P.E.

LECTURE 10: JACOBI SYMBOL

Math 100 Review Sheet

Total Score Maximum

Mathematics Extension 1

In Mathematics for Construction, we learnt that

Prof. Anchordoqui. Problems set # 4 Physics 169 March 3, 2015

SAINT IGNATIUS COLLEGE

Practice Problems for the First Midterm

Dynamics: Newton s Laws of Motion

Instructor(s): Acosta/Woodard PHYSICS DEPARTMENT PHY 2049, Fall 2015 Midterm 1 September 29, 2015

Math 113 Exam 1-Review

CE 160 Lab 2 Notes: Shear and Moment Diagrams for Beams

Stress distribution in elastic isotropic semi-space with concentrated vertical force

A-Level Mathematics Transition Task (compulsory for all maths students and all further maths student)

1.2 What is a vector? (Section 2.2) Two properties (attributes) of a vector are and.

A LEVEL TOPIC REVIEW. factor and remainder theorems

Mathematics Extension 2

MATH 253 WORKSHEET 24 MORE INTEGRATION IN POLAR COORDINATES. r dr = = 4 = Here we used: (1) The half-angle formula cos 2 θ = 1 2

Job No. Sheet 1 of 8 Rev B. Made by IR Date Aug Checked by FH/NB Date Oct Revised by MEB Date April 2006

Phys101 Lecture 4,5 Dynamics: Newton s Laws of Motion

Definition of Continuity: The function f(x) is continuous at x = a if f(a) exists and lim

Partial Differential Equations

l 2 p2 n 4n 2, the total surface area of the

Trigonometric Functions

Lecture 8. Newton s Laws. Applications of the Newton s Laws Problem-Solving Tactics. Physics 105; Fall Inertial Frames: T = mg

Chapter 0. What is the Lebesgue integral about?

Physics 9 Fall 2011 Homework 2 - Solutions Friday September 2, 2011

ES 111 Mathematical Methods in the Earth Sciences Lecture Outline 1 - Thurs 28th Sept 17 Review of trigonometry and basic calculus

BEAM DIAGRAMS AND FORMULAS. Nomenclature

Columns and Stability

SUPPLEMENTARY INFORMATION

ROTATION IN 3D WORLD RIGID BODY MOTION

To Do. Vectors. Motivation and Outline. Vector Addition. Cartesian Coordinates. Foundations of Computer Graphics (Spring 2010) x y

Correct answer: 0 m/s 2. Explanation: 8 N

Math 426: Probability Final Exam Practice

Section 4.7 Inverse Trigonometric Functions

Math 231E, Lecture 33. Parametric Calculus

A. Limits - L Hopital s Rule ( ) How to find it: Try and find limits by traditional methods (plugging in). If you get 0 0 or!!, apply C.! 1 6 C.

Physics 105 Exam 2 10/31/2008 Name A

USA Mathematical Talent Search Round 1 Solutions Year 25 Academic Year

Eigen Values and Eigen Vectors of a given matrix

Physics 241 Exam 1 February 19, 2004

Version 001 HW#6 - Circular & Rotational Motion arts (00223) 1

Physics 110. Spring Exam #1. April 16, Name

a < a+ x < a+2 x < < a+n x = b, n A i n f(x i ) x. i=1 i=1

Chapter 2. Vectors. 2.1 Vectors Scalars and Vectors

THE DISCRIMINANT & ITS APPLICATIONS

Supplement 4 Permutations, Legendre symbol and quadratic reciprocity

Transcription:

Subfculty of Civil Engineering rk ech ge with your: Structurl echnics STUDENT NUBER : NAE : Em CT309 STRUCTURAL ECHANICS 4 ril 0, 09:00 :00 hours This em consists of 4 roblems. Use for ech roblem serte sheet of er. Do not forget to mention your nme nd number on ech er. Work net nd tidy, the qulity of the resenttion cn be used in the grding. The use of Phone s or comuters, PDA s nd /or Wifi or Blue Tooth equiment is not llowed. Turn off the equiment nd remove it from your tble. A scientific (rogrmmble) clcultor is llowed All required formuls cn be found on the lst ges of this em Kee n eye on the clock nd use the secified times er roblem s guidnce.

Em CT309 Structurl echnics 4 r 0 Problem : Plsticity ( 45 min ) In the following figure frme is shown which is fied in A nd suorted in B with horizontl roller. Concentrted forces ct t D nd E in the directions shown. Segment ACD hs twice the strength of segment BED. C D E 3 A B Questions: ) Determine the ossible collse mechnisms nd show these with smll sketches. b) Comute the collse lod nd rove the uniqueness of your solution. c) Show the moment distribution t the moment of collse. - -

Em CT309 Structurl echnics 4 r 0 Problem : Influence lines ( 35 min ) The stticlly determinte hinged bem structure form the figure below consists of three bems which re connected though hinges t S nd S. A B S S C D -s z-s 5,0 m,0 m 3,0 m 3,0 m 3,0 m igure : Sttic determinte hinged bem Questions: ) Elin how n influence line for force quntity cn be determined. b) Elin how n influence line for dislcement quntity cn be determined. c) Construct the influence line for the moment t B. d) Construct the influence line for the moment t C. e) Construct the influence line for the sher force directly to the left of C. f) Construct the influence line for the sher force t mid sn of sn AB. g) Construct the influence line for the for the suort rection t C. h) Sketch the influence line for the dislcement of hinge S. i) rk the osition of constnt distributed lod on the structure in order to mimize the bending moment t one of the suorts. - 3 -

Em CT309 Structurl echnics 4 r 0 Problem 3 : work nd energy methods ( 45 min ) A hinged bem with rottionl sring ttched t A is loded by concentrted lod nd distributed lod q. S is hinge connecting the two bem rts loded in bending. The bending stiffness for the totl structure is constnt nd denoted with. The sring stiffness cn be eressed in terms of the bending stiffness by using dimensionless sclr: r ρ ρ r The deformtion energy stored in rottionl sring cn be eressed s: E v r veer r S q A B C Questions: ) ind the moment distribution fort his structure nd drw this oment-line. b) ind the verticl dislcement of the hinge S with work or energy method. Write the dislcement in terms of the given rmeters nd use the given sclr ρ for the stiffness of rottionl sring. c) Secify the mount of deformtion energy stored in the structure due to the secified lod nd eress this in terms of the rmeters, q,, ρ en. d) ind for : 0000 knm ; ρ, 4 m; q 4 kn/m nd 0 kn the deflection t S in mm nd the mimum moment in knm. e) ind the mount of deformtion energy for very smll vlues of r. HINT : use sketch of the deformed structure! - 4 -

Em CT309 Structurl echnics 4 r 0 Problem 4 ( 45 min ) An element subject to bending nd sher is comosition of two mterils. The geometry of the cross section is symmetricl nd shown in the figure below. Both mterils re erfectly bonded nd the cross section cn be regrded s n inhomogeneous cross section. The dimensions nd Young s moduli of the mterils cn be found below. The bem is coincides with the -is nd the origin of the coordinte system is tken t the norml force center of the cross section. The cross section is loded in the -z-vlk with sher force of 9 kn nd bending moment of 90 knm. y NC? mteril mteril R S z U T Given : 3 E 00 0 N/mm ; 3 E 800 0 N/mm ; 300 mm Questions: ) Why is the origin of the coordinte system tken t the norml force center? b) ind the loction of the norml force center. c) The constitutive mtri of the cross section is given below. Show the correctness of this mtri. 0, 6 0 0 0 080 430 0 0 430 080 units N, mm d) ind the osition of the neutrl is, the lne of loding m nd the lne of curvture k nd drw these lines in one grh. e) Show in second grh the stress distribution of the cross section for both mterils. f) ind the totl longitudinl force in the interfce RST between mteril nd er unit of length. g) ind the most outer left oint of the kernel of this cross section nd mrk this oint in one of the grhs of the cross section. h) In which lne will this cross section hve the mimum bending stiffness nd wht is the mgnitude (vlue) of this stiffness? - 5 -

Em CT309 Structurl echnics 4 r 0 ORULAS Inhomogeous nd/or unsymmetricl cross sections : ε ( y, z) ε + κ y + κ z nd: σ ( y, z) E( y, z) ε ( y, z) y z y yy yz κ y ey yy yz / y nd κ e EA / z z yz zz z z yz zz V ES s s V ( ) ( ) ( ) ( ) ( ) y y VzESz ( ) R s ; or: ; σ t ( ) yy zz b yz tn α ; + ± + ( ) ( yy zz ) ( ) ( ) ( ), yy zz yy zz yz Deformtion energy: Kinemtic reltions: du Ev EAε d (etension) ε d Ev κ d (bending) d w κ d Comlementiry energy: Constitutive reltions: N Ec d (etensie) EA N EA. ε. κ Ec d (buiging) Cstiglino s theorem s: Work method with unit lod: Ev Ec ( ) m( ) d i ui u u i i - 6 -

Em CT309 Structurl echnics 4 r 0-7 -

Em CT309 Structurl echnics 4 r 0-8 -

Em CT309 Structurl echnics 4 r 0 Problem : Plsticity ANSWERS ) The given structure is stticlly indeterminte with degree of one. To obtin mechnism, two dditionl hinges re required. Hinges cn occur t four ositions. Thus, si mechnisms hve to be investigted. However, moments cn not occur t E due to the loding nd suort conditions t B thus only three mechnisms re left to be considered. Possible mechnisms re shown below. Ech mechnism is shown in detil on the following ges. 3 4 5 4 9-9 -

Em CT309 Structurl echnics 4 r 0 θ 5θ δ A 0 4 δθ δθ 0(!) + 5δθ 0 5 θ θ δ A 0 4 δθ δθ δθ + δθ + 7δθ 0 9-0 -

Em CT309 Structurl echnics 4 r 0 θ θ θ 3 δ A 0 δθ δθ δθ + δθ + δθ 0 ) The ultimte lod is the lowest lod found: 4 9 0,444 b) To find the correct moment distribution strt with the suort rections. The moment distribution shows stticlly dmissible distribution in which t no cross section the bending moments eceeds the utltimte lstic ccity of the cross section. (uniqueness theorem) 9 4 9 7 8 8 - -

Em CT309 Structurl echnics 4 r 0 Problem : Influence lines A B S S C D -s z-s 5,0 m,0 m 3,0 m 3,0 m 3,0 m,0 q q q B m, q 5 5,0 i-lijn B q (etreme loding) 3,0 q q 3 6 9 C m, q,0 i-lijn C,0 i-lijn V C-L 0,5 0,4 i-lijn V AB 0,5 i-lijn C V,0,0,0 i-lijn A V 8/ - -

Em CT309 Structurl echnics 4 r 0 Problem 3 : Work nd Energy ethods ) The moment distribution cn be found bse don equilibrium. The distributed lod q is in fct blnced thus only the concentrted lod is contributing to the moment in the sring nd the member AS. ( first yers knowledge!!) r ρ ρ r r S q A B C Q 7 knm -line due to nd q -line due to Q 40 r Q S q b) To find the dislcement t S dummy lod Q is required. In red the moment distribution due to the dummy lod is resented. Since the moment distribution over SB nd BC re ehibiting mirror symmetry, only rt SB hs to be emined. Using locl coordinte for rt AS nd SB denoted with nd, the deformtion energy cn esily be eressed in terms of, q nd Q : (( )( )) + q Q v 0 0 Ev + d + d r ( Q) v met: Using Cstiglino s theorem solves the deflection t S: (note: nd integrl is irrelevnt) w S A ( ) ( ) E Q Q v Q ρ 3 3 3 The dummy lod is zero which results in: Hinge S will move uwrds due tot the lod. w S 3 3 3 (3 + ρ) 3ρ ρ 3 c) Using the given vlues results in dislcement of 0,0533 m uwrds. This dislcement is indeendent of the distributed lod q! B - 3 -

Em CT309 Structurl echnics 4 r 0 d) The totl deformtion energy stored due to the loding is: (note : nd integrl is essentil) + q ( ( )) v 0 0 Ev + d + d r E v ( 0 ( + ρ) + ρ(5 + ρ ) 3 q q 0ρ e) If the sring stiffness becomes very smll, oint A turns into hinge. A mechnism will occur. The lod cn move infinitely nd thus roduce infinite work. The bending deformtion will be smll comred to the deformtion energy stored in the sring. So rcticlly ll deformtion energy hs to be tken by the sring(!) which results in hrdly ny deformtion energy (nd curvture) in the elements loded in bending. The brs will remin stright: E ( ) w r v lim ρ 0-4 -

Em CT309 Structurl echnics 4 r 0 Problem 4 : Non-symmetricl cross sections ) See the lecture notes. b) The il stiffness of the cross section cn be found with: EA E E + E 6 0 The origin of the coordinte system used is locted t the NC. The verticl osition of the NC with resect to the uer side of the cross section is: z NC 400 mm The horizontl osition with resect to the left side of the cross section is: y NC 00 mm c) The cross sectionl constitutive reltion reltes the sectionl forces to the deformtions if the cross section. The bending stiffnesses cn be found using the strtegy outlined in the lecure notes. This emle is very bsic so only nswers re resented here: N EA 0 0 ε y 0 yy yz κ y cross sectionl constitutive reltion [N, mm] z 0 yz zz κ z 0, 6 0 0 0 K 0 0 430 080 f 0 6 0 080 430 90 0 d) Since this structure is loded in bending only, the strin ε t the NC must be zero. The curvtures cn be found with the constitutive reltion: N ε 0 EA κ 0,79 0 ( ) y zz y yz z yy zz yz κ + 0, 476 0 ( ) z yz y yy z yy zz yz The direction of the lne of loding nd the lne of curvture cn be obtined with: κ α α α α z o z o tn m m 90 ; tn k k 76 y κ y The stresses for ech oint of the cross section cn be comuted with: σ ( y, z) E ( ε + κ y + κ z) N/mm y z The neutrl is n.. cn lso be found with this ltter eression by: ε ( y, z) ε + κ y + κ z 0 κ y + κ z 0 y 4z 0 y z y z e) The stress distribution cn be visulized with few oints. Only the four vlues mrked in bold in the tble on the net ge were essentil for the grhs. - 5-9 6 6

Em CT309 Structurl echnics 4 r 0 Tbel : Stress in the secified oints teril oint y [mm] z [mm] E [N/mm ] Stress [N/mm ] R 00-00 00000-4, S -00-00 00000-7, T -00 00 00000, V -400 00 00000 8,3 W -400-400 00000-8,3 X 00-400 00000-4,4 R 00-00 800000-7,3 S -00-00 800000-63,7 T -00 00 800000 9,0 U 00 00 800000 7,3 The neutrl is goes through the NC since the norml force N is zero. The red stress distribution reresents the stresses in mteril nd the blue one reresents mteril. The moment nd thus the lod cts in the -m lne. The curvture κ cts in the -k lne. f) The longitudinl force er unit length of bem in the interfce between mteril nd cn be obtined with: 7 n 4 - + 8 mteril 9 y X R U k NC m mteril S T z W n V teril (RSTU) is tken s the sliding element with cross sectionl re (): ( ) ( σ σ σ σ ) ( ) R 4 R S T U s V Vz z s + + + 4 7,3 300 300 3 6 9 0 86 N/mm 90 0 g) The outer left kern oint cn be found by tking neutrl is long VW. The loction of the kernel oint cn be found with: ey yy yz /( 400) 50 mm e z EA yz zz 0,5 h) The rincile direction of this cross section is t n ngle of 45 degrees. or the rincile coordinte system this cross section hs one is of symmetry. The mimum stiffness of this section then becomes: ( ) ( ) ( ) + ± +, yy zz yy zz yz 5400 0 Nmm ; 340 0 Nmm imum bending stiffness is therefore 5400 0 Nmm. - 6 - k