Mechanics of Solids I Columns. Stability of Structures oIn the design of columns, cross-sectional area is selected such that  allowable stress is not.

Slides:



Advertisements
Similar presentations
CHAPTER OBJECTIVES Discuss the behavior of columns.
Advertisements

Beam-Columns.
Spring 2007 Dr. D. M. McStravick Rice University
By: Prof Dr. Akhtar Naeem Khan
Indeterminate Structure Session Subject: S1014 / MECHANICS of MATERIALS Year: 2008.
Introduction to Axially Loaded Compression Members
2E4: SOLIDS & STRUCTURES Lecture 15 Dr. Bidisha Ghosh Notes: lids & Structures.
Mechanics of Materials – MAE 243 (Section 002) Spring 2008
Beams and Frames.
10 Columns.
Engineering materials lecture #14
LRFD-Steel Design Dr. Ali Tayeh Second Semester
Chapter 13 Buckling of Columns
Compression Members. Compression Members: Structural elements subjected only to axial compressive forces Stress:Uniform over entire cross section.
Column Design ( ) MAE 316 – Strength of Mechanical Components
Buckling Phenomena. Stability of Structures P< Elastic Hinge Analysis of Column (independent of  ) (How to find k?)
Buckling Critical Load Considerations
Compression Members.
Compression Members.
Deflection and Stiffness
BFC (Mechanics of Materials) Chapter 5: Compression Member
Copyright © 2011 Pearson Education South Asia Pte Ltd
ENGR 220 Section 13.1~13.2.
Axially loaded member Axial load and normal stress under equilibrium load, Elastic Deformation.
MECHANICS OF MATERIALS 7th Edition
CHAPTER OBJECTIVES Discuss the behavior of columns.
Dr. Ali I. Tayeh First Semester
Mukavemet II Strength of Materials II
10 Columns.
Reinforced Concrete Design
Chapter 10 Columns .
FINITE ELEMENT ANALYSIS CONVERSION FACTORS FOR NATURAL VIBRATIONS OF BEAMS Austin Cosby and Ernesto Gutierrez-Miravete Rensselaer at Hartford.
Mechanics of Materials – MAE 243 (Section 002) Spring 2008
© Dr S R Satish Kumar, IIT Madras1 SECTION 7 DESIGN OF COMPRESSION MEMBERS.
Chapter Outline Shigley’s Mechanical Engineering Design.
Chapter 1: Stress Review important principles of statics
Civil Engineering Materials – CIVE 2110
Load and Stress Analysis
Workshop at Indian Institute of Science 9-13 August, 2010 Bangalore India Fire Safety Engineering & Structures in Fire Organisers:CS Manohar and Ananth.
LRFD- Steel Design Dr. Ali I. Tayeh second Semester Dr. Ali I. Tayeh second Semester.
Buckling of Slender Columns ( )
COMPERSION MEMBER.  An initially straight strut or column, compressed by gradually increasing equal  and opposite axial forces at the ends is considered.
Buckling Capacity of Pretwisted Steel Columns: Experiments and Finite Element Simulation Farid Abed & Mai Megahed Department of Civil Engineering American.
Copyright Kaplan AEC Education, 2005 Mechanics of Materials Outline Overview AXIALLY LOADED MEMBERS, p. 262 Modulus of Elasticity Poisson’s Ratio Thermal.
Strength of Materials Malayer University Department of Civil Engineering Taught by: Dr. Ali Reza Bagherieh In The Name of God.
Stress and Strain ( , 3.14) MAE 316 – Strength of Mechanical Components NC State University Department of Mechanical & Aerospace Engineering Stress.
Unit-5. Torsion in Shafts and Buckling of Axially Loaded Columns Lecture Number-5 Mr. M. A.Mohite Mechanical Engineering S.I.T., Lonavala.
Strength of Materials I EGCE201 กำลังวัสดุ 1 Instructor: ดร. วรรณสิริ พันธ์อุไร ( อ. ปู ) ห้องทำงาน : 6391 ภาควิชาวิศวกรรมโยธา
☻ ☻ ☻ ☻ 2.0 Bending of Beams sx 2.1 Revision – Bending Moments
Chapter 5 Introduction to Axially Loaded Compression Members.
Engg College Tuwa Mechanics of Solids.( ) Presented by: PARMAR CHETANKUMAR VIKRAMSINH PARMAR NILESHKUMAR NATVARLAL PARMAR.
Mechanics of Solids (M2H321546)
Poisson’s Ratio For a slender bar subjected to axial loading:
10 Columns.
Buckling & Stability Critical Load
contents Design of beams (week 11,12,13), (10,17,24 Nov.)
Unit-5. Torsion in Shafts and Buckling of Axially Loaded Columns
Poisson’s Ratio For a slender bar subjected to axial loading:
Revision for Mechanics of Materials
13.3 Columns with Various Types of Supports:
Compression Members.
Buckling & Stability Critical Load
Ch. 2: Fundamental of Structure
Chapter 3 Buckling of Column SAIFULNIZAN JAMIAN.
Compression Test of Steel Columns
PLASTIC ANALYSIS OF STRUCTURES
10 Columns.
Poisson’s Ratio For a slender bar subjected to axial loading:
Mechanics of Materials Engr 350 – Lecture 38 Columns
BUCKLING OF COLUMNS. AIM To study the failure analysis of buckling of columns.
Presentation transcript:

Mechanics of Solids I Columns

Stability of Structures oIn the design of columns, cross-sectional area is selected such that  allowable stress is not exceeded  deformation falls within specifications oAfter these design calculations, one may discover that the column is unstable under loading and that it suddenly becomes sharply curved or buckles.

Stability of Structures oConsider model with two rods and torsional spring. After a small perturbation, oColumn is stable (tends to return to aligned orientation) if

StabilityofStructures Stability of Structures oAssume that a load P is applied. After a perturbation, the system settles to a new equilibrium configuration at a finite deflection angle. oNoting that sin  P cr.

Euler’s Formula for Pin-Ended Beams oConsider an axially loaded beam. After a small perturbation, the system reaches an equilibrium configuration such that oSimilar to D.E. for simple harmonic motion (except for variable x instead of t) oSet, general solution is in the form

Euler’s Formula for Pin-Ended Beams oApply boundary conditions and thus oSolution with assumed configuration can only be obtained if oSmallest P (critical load) is obtained for n = 1 and I = I min

Euler’s Formula for Pin-Ended Beams oThe value of stress corresponding to the critical load, oPreceding analysis is limited to centric loadings.

Extension of Euler’s Formula oA column with one fixed and one free end, will behave as the upper-half of a pin-connected column. oThe critical loading is calculated from Euler’s formula,

Extension of Euler’sFormula Extension of Euler’s Formula

Problem10.1 Problem 10.1 oAn aluminum column of length L and rectangular cross section has a fixed end at B and supports a centric load at A. Two smooth and rounded fixed plates restrain end A from moving in one of the vertical planes of symmetry but allow it to move in the other plane. a)Determine the ratio a/b of the two sides of the cross section corresponding to the most efficient design against buckling. b)Design the most efficient cross section for the column. L = 0.5 m E = 70 GPa P = 20 kN FS = 2.5

Problem 10.1 Buckling in xy plane: Buckling in xz plane: Most efficient design: SOLUTION: The most efficient design occurs when the resistance to buckling is equal in both planes of symmetry. This occurs when the slenderness ratios are equal.

Problem 10.1 L = 0.5 m E = 70 GPa P = 20 kN FS = 2.5 a/b = 0.35 Design: