THEORY OF STRUCTURES CHAPTER 3 : SLOPE DEFLECTION (FOR FRAME) PART 2

Similar documents
THEORY OF STRUCTURES CHAPTER 3 : SLOPE DEFLECTION (FOR BEAM) PART 1

SLOPE-DEFLECTION METHOD

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

MECHANICS OF MATERIALS

Chapter 11. Displacement Method of Analysis Slope Deflection Method

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

UNIT-IV SLOPE DEFLECTION METHOD

Module 3. Analysis of Statically Indeterminate Structures by the Displacement Method. Version 2 CE IIT, Kharagpur

MECHANICS OF MATERIALS. Analysis of Beams for Bending

The bending moment diagrams for each span due to applied uniformly distributed and concentrated load are shown in Fig.12.4b.

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

CITY AND GUILDS 9210 UNIT 135 MECHANICS OF SOLIDS Level 6 TUTORIAL 5A - MOMENT DISTRIBUTION METHOD

UNIT II SLOPE DEFLECION AND MOMENT DISTRIBUTION METHOD

Example 17.3 Analyse the rigid frame shown in Fig a. Moment of inertia of all the members are shown in the figure. Draw bending moment diagram.

SAB2223 Mechanics of Materials and Structures

TYPES OF STRUCUTRES. HD in Civil Engineering Page 1-1

P.E. Civil Exam Review:

Determinate portal frame

Where and are the factored end moments of the column and >.

Method of Consistent Deformation

Chapter 8 Deflection. Structural Mechanics 2 Dept of Architecture

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

QUESTION BANK ENGINEERS ACADEMY. Hinge E F A D. Theory of Structures Determinacy Indeterminacy 1

MODULE 3 ANALYSIS OF STATICALLY INDETERMINATE STRUCTURES BY THE DISPLACEMENT METHOD

Chapter 4.1: Shear and Moment Diagram

Moment Distribution Method

Continuous Beams - Flexibility Method

UNIT IV FLEXIBILTY AND STIFFNESS METHOD

FORMULA FOR FORCED VIBRATION ANALYSIS OF STRUCTURES USING STATIC FACTORED RESPONSE AS EQUIVALENT DYNAMIC RESPONSE

Deflection of Beams. Equation of the Elastic Curve. Boundary Conditions

k 21 k 22 k 23 k 24 k 31 k 32 k 33 k 34 k 41 k 42 k 43 k 44

REINFORCED CONCRETE DESIGN 1. Design of Column (Examples and Tutorials)

Lecture 11: The Stiffness Method. Introduction

Preliminaries: Beam Deflections Virtual Work

Module 4 : Deflection of Structures Lecture 4 : Strain Energy Method

UNIT-V MOMENT DISTRIBUTION METHOD

STRUCTURAL ANALYSIS BFC Statically Indeterminate Beam & Frame

MECHANICS OF MATERIALS

Due Tuesday, September 21 st, 12:00 midnight

INFLUENCE LINE. Structural Analysis. Reference: Third Edition (2005) By Aslam Kassimali

Shear force and bending moment of beams 2.1 Beams 2.2 Classification of beams 1. Cantilever Beam Built-in encastre' Cantilever

, and M A , R B. , and then draw the shear-force and bending-moment diagrams, labeling all critical ordinates. Solution 10.

External work and internal work

Unit-II ENGINEERING MECHANICS

7 STATICALLY DETERMINATE PLANE TRUSSES

INTRODUCTION (Cont..)

Chapter 7. ELASTIC INSTABILITY Dr Rendy Thamrin; Zalipah Jamellodin

A study of the critical condition of a battened column and a frame by classical methods

Finite Element Modelling with Plastic Hinges

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


7.4 The Elementary Beam Theory

Slenderness Effects for Concrete Columns in Sway Frame - Moment Magnification Method (CSA A )

Structural Analysis Lab


Plastic Analysis 3rd Year Structural Engineering

Structural Analysis III Moment Distribution

QUESTION BANK. SEMESTER: V SUBJECT CODE / Name: CE 6501 / STRUCTURAL ANALYSIS-I

PROBLEM 5.1. wl x. M ( Lx x )

6. KANIS METHOD OR ROTATION CONTRIBUTION METHOD OF FRAME ANALYSIS

MODULE C: COMPRESSION MEMBERS

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

Influence lines for statically indeterminate structures. I. Basic concepts about the application of method of forces.

BOOK OF COURSE WORKS ON STRENGTH OF MATERIALS FOR THE 2 ND YEAR STUDENTS OF THE UACEG

Lecture 8: Flexibility Method. Example

Structural Analysis III Moment Distribution

DEFLECTION CALCULATIONS (from Nilson and Nawy)

Types of Structures & Loads

BEAMS: SHEAR AND MOMENT DIAGRAMS (FORMULA)

Methods of Analysis. Force or Flexibility Method

Prof. Dr. Zahid Ahmad Siddiqi BEAM COLUMNS

Internal Internal Forces Forces

Moment Area Method. 1) Read

Workshop 8. Lateral Buckling

ARCE 302-Structural Analysis

DESIGN OF END PLATE JOINTS SUBJECT TO MOMENT AND NORMAL FORCE

NOVEL FLOWCHART TO COMPUTE MOMENT MAGNIFICATION FOR LONG R/C COLUMNS

MECHANICS OF MATERIALS

FRAME ANALYSIS. Dr. Izni Syahrizal bin Ibrahim. Faculty of Civil Engineering Universiti Teknologi Malaysia

FORMULATION OF THE INTERNAL STRESS EQUATIONS OF PINNED PORTAL FRAMES PUTTING AXIAL DEFORMATION INTO CONSIDERATION

StaticS Fourteenth edition in si units

Multi Linear Elastic and Plastic Link in SAP2000

2 marks Questions and Answers

MECHANICS OF MATERIALS

Chapter 4-b Axially Loaded Members

Bracing for Earthquake Resistant Design

Chapter 2: Rigid Bar Supported by Two Buckled Struts under Axial, Harmonic, Displacement Excitation..14

14. *14.8 CASTIGLIANO S THEOREM

Shear Force V: Positive shear tends to rotate the segment clockwise.

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

Portal Frame Calculations Lateral Loads


BEAM A horizontal or inclined structural member that is designed to resist forces acting to its axis is called a beam

Supplementary Information for Design of Bending Multi-Layer Electroactive Polymer Actuators

METHOD OF COMPUTING GEOMETRIC RELATIONS IN STRUCTURAL ANALY IS

BTU 1113 Physics. Chapter 2: Kinematics. by Nadzirah Bte Mohd Mokhtar Faculty of Engineering Technology

Lecture 7: The Beam Element Equations.

ENGINEERING MECHANICS BAA1113. Chapter 4: Force System Resultants (Static)

Assumptions: beam is initially straight, is elastically deformed by the loads, such that the slope and deflection of the elastic curve are

ENGI 1313 Mechanics I

Transcription:

or updated version, please click on http://ocw.ump.edu.my THEORY O STRUTURES HAPTER : SOPE DEETION (OR RAE) PART by Saffuan Wan Ahmad aculty of ivil Engineering & Earth Resources saffuan@ump.edu.my

hapter : Part Slope Deflection Aims Determine the end moment for frame using Slope Deflection ethod. Expected Outcomes : Able to identify the frame with or without side sway. Able to determine end moment at critical points. References echanics of aterials, R.. Hibbeler, 7th Edition, Prentice Hall Structural Analysis, Hibbeler, 7th Edition, Prentice Hall Structural Analysis, SI Edition by Aslam Kassimali,engage earning Structural Analysis, oates, oatie and Kong Structural Analysis - A lassical and atrix Approach, Jack. cormac and James K. Nelson, Jr., 4th Edition, John Wiley

RAE WITH SIDE SWAY WITHOUT SIDE SWAY Displace to the side when the body or the loading acting on it is nonsymmetric Properly restrained Symmetric with respect both loading and geometry

EER SIZES DEPEND ON ONIGURATION OADING SYSTE SUPPORT SYSTE

RAE WITHOUT SIDESWAY RAE WITH SIDESWAY

EXAPE 1 ANAYSIS - RAE WITHOUT SIDESWAY. y using SD, determine the bending moment at critical points. Assume is constant.

SOUTION IXED END OENT PQ QP RS SR 0 QR RQ P 8 P 8 45(6) 8 45(6) 8.75 knm.75 knm

SOPE DEETION EQUATION P 0 S PQ 4 6 P Q PQ PQ Q QP QP Q P 4 Q 6 QP

.75 R Q QR.75 Q R RQ RQ Q R RQ 6 4 QR R Q QR 6 4

RS 4 6 R S RS RS R SR 4 6 S R SR SR R

EQUIIRIU AT JOINT Q 0 R 0 QP 4 RQ Q 4 R QR RS R Q 0 0.75.75 1

4 1 1 4 Q R.75.75 Y USING AUATOR Q R.75.75

SUSTITUTING INTO SDE PQ QP QR RQ RS SR 11.5kNm.5kNm.5kNm.5kNm.5kNm 11.5kNm

OOD O IND Determine end moment at critical point. 10kN/m 6m A D m m

SOUTION IXED END OENT A A D D 0 0kNm SOPE DEETION EQUATION A 0 D A ( ) A A A

A A A ) ( 4 A 0

D D D ) ( 4 D 0

D D D ) ( D EQUIIRIU AT JOINT 0 0 0 0 D A

1 1 0 0 Solving by using alculator 18 18

SUSTITUTING INTO SDE A A D D 1kNm 4kNm 4kNm 4kNm 4kNm 1kNm

ANAYSIS O RAE WITH SIDE SWAY. EER SIZES DEPEND ON ONIGURATION OADING SYSTE SUPPORT SYSTE

UNDAENTA ASSUPTIONS 1. That axial deformation is ignored. That transverse end displacement do not affect the member length A A

EXAPE DETERINE END OENT AT RITIA POINT. ASSUE IS ONSTANT. 00 kn 4m 6m A D 5m

00 kn 4m 6m A D 5m

SOUTION ixed End oment A A D D 0 SOPE DEETION EQUATION A 8 A 8

4 5 5 5 5 5 D 6 D 6

Equilibrium at joint 0 A 0 4 8 5 5 9 0 5 5 8 0 1

0 D 0 4 0 5 5 6 0 5 15 6

H 0 H A H D 00 0 onsider member A H A 0 A A H A (4) 0 H A A A H A A 4 A

onsider member D H D 0 D D H D (6) 0 H D D H D D 6 D

6 A A A 4 6 A D 6 4 D D 4 00 D 4800 Insert the value 1 5 9 4800 6

ATRIX OR 4800 0 0 6 5 1 9 6 1 15 5 8 5 5 9 Solving by using calculator 150.86 75.66 4.78

Substituting into SDE A A D D 4.78 (150.88) 47.16kNm 8 (150.88) 4.78 5.9kNm 8 4(4.78) (75.66) 5.9kNm 5 5 4(75.66) (4.78) 158.04kNm 5 5 (75.66) 150.88 158.04kNm 6 75.66 150.88 18.6kNm 6

THANKS

Author Information ohd Arif in Sulaiman ohd aizal in d. Jaafar ohammad Amirulkhairi in Zubir Rokiah inti Othman Norhaiza inti Ghazali Shariza inti at Aris