Moments of Inertia. Notation:

Similar documents
Statics: Lecture Notes for Sections 10.1,10.2,10.3 1

2. Supports which resist forces in two directions. Fig Hinge. Rough Surface. Fig Rocker. Roller. Frictionless Surface

Centroids & Moments of Inertia of Beam Sections

Distributed Forces: Moments of Inertia

ME 141. Lecture 8: Moment of Inertia

BEAMS: SHEAR AND MOMENT DIAGRAMS (FORMULA)

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

ME 201 Engineering Mechanics: Statics

10.5 MOMENT OF INERTIA FOR A COMPOSITE AREA

STATICS. Moments of Inertia VECTOR MECHANICS FOR ENGINEERS: Seventh Edition CHAPTER. Ferdinand P. Beer

Moment of Inertia and Centroid

Lecture 6: Distributed Forces Part 2 Second Moment of Area

Second Moments or Moments of Inertia

Chapter 10: Moments of Inertia

ME 101: Engineering Mechanics

CIVL Statics. Moment of Inertia - Composite Area. A math professor in an unheated room is cold and calculating. Radius of Gyration

Chapter 6: Cross-Sectional Properties of Structural Members

Statics: Lecture Notes for Sections

ENGI 4430 Multiple Integration Cartesian Double Integrals Page 3-01

AREAS, RADIUS OF GYRATION

SOLUTION Determine the moment of inertia for the shaded area about the x axis. I x = y 2 da = 2 y 2 (xdy) = 2 y y dy

Hong Kong Institute of Vocational Education (Tsing Yi) Higher Diploma in Civil Engineering Structural Mechanics. Chapter 2 SECTION PROPERTIES

ENGI 4430 Advanced Calculus for Engineering Faculty of Engineering and Applied Science Problem Set 3 Solutions [Multiple Integration; Lines of Force]

Properties of Sections

ARCH 631 Note Set 2.1 F2010abn. Statics Primer

Beam Bending Stresses and Shear Stress

Chapter 9 Moment of Inertia

Moment of Inertia. Moment of Inertia

Chapter 9 BIAXIAL SHEARING

Sub:Strength of Material (22306)

Moments and Product of Inertia

MOMENTS OF INERTIA FOR AREAS, RADIUS OF GYRATION OF AN AREA, & MOMENTS OF INTERTIA BY INTEGRATION

REVOLVED CIRCLE SECTIONS. Triangle revolved about its Centroid

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

Centers of Gravity - Centroids

[8] Bending and Shear Loading of Beams

CH. 4 BEAMS & COLUMNS

STATICS VECTOR MECHANICS FOR ENGINEERS: Distributed Forces: Centroids and Centers of Gravity. Tenth Edition CHAPTER

Mechanics of Solids notes

UNIT- I Thin plate theory, Structural Instability:

10 3. Determine the moment of inertia of the area about the x axis.

ENGR-1100 Introduction to Engineering Analysis. Lecture 17

[4] Properties of Geometry

ENGI Multiple Integration Page 8-01

DEFINITION OF MOMENTS OF INERTIA FOR AREAS, RADIUS OF GYRATION OF AN AREA

Chapter 5 Equilibrium of a Rigid Body Objectives

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

h p://edugen.wileyplus.com/edugen/courses/crs1404/pc/b03/c2hlch...

8.3 Shear and Bending-Moment Diagrams Constructed by Areas

CH. 5 TRUSSES BASIC PRINCIPLES TRUSS ANALYSIS. Typical depth-to-span ratios range from 1:10 to 1:20. First: determine loads in various members

TWISTING (TORSIONAL) STIFFNESS. Barry T. Cease Cease Industrial Consulting

Strength of Materials Prof. Dr. Suraj Prakash Harsha Mechanical and Industrial Engineering Department Indian Institute of Technology, Roorkee

Bending Stress. Sign convention. Centroid of an area

Stresses in Curved Beam

5. What is the moment of inertia about the x - x axis of the rectangular beam shown?

Shear Stress. Horizontal Shear in Beams. Average Shear Stress Across the Width. Maximum Transverse Shear Stress. = b h

Centroid & Moment of Inertia

CHAPTER 4. Stresses in Beams

Mechanics of Materials

Engineering Mechanics: Statics in SI Units, 12e

4.5 The framework element stiffness matrix

Engineering Tripos Part IIA Supervisor Version. Module 3D4 Structural Analysis and Stability Handout 1

Determine the moment of inertia of the area about the x axis Determine the moment of inertia of the area about the y axis.

Supplement: Statically Indeterminate Frames

This procedure covers the determination of the moment of inertia about the neutral axis.

Statics Primer. Notation:

2015 ENGINEERING MECHANICS

EMA 3702 Mechanics & Materials Science (Mechanics of Materials) Chapter 6 Shearing Stress in Beams & Thin-Walled Members

Mechanics of Materials Primer

POE Practice Test - Materials


1. Given the shown built-up tee-shape, determine the following for both strong- and weak-axis bending:

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

APRIL Conquering the FE & PE exams Formulas, Examples & Applications. Topics covered in this month s column:

The standard form of the equation of a circle is based on the distance formula. The distance formula, in turn, is based on the Pythagorean Theorem.

Rigid and Braced Frames

REVIEW FOR EXAM II. Dr. Ibrahim A. Assakkaf SPRING 2002

Chapter (6) Geometric Design of Shallow Foundations

Consider a cross section with a general shape such as shown in Figure B.2.1 with the x axis normal to the cross section. Figure B.2.1.

Chapter 4 Pure Bending

ENG202 Statics Lecture 16, Section 7.1

Beam Design and Deflections

Unit 15 Shearing and Torsion (and Bending) of Shell Beams

Two small balls, each of mass m, with perpendicular bisector of the line joining the two balls as the axis of rotation:

National Exams May 2015

Beams III -- Shear Stress: 1

Introduction to Structural Member Properties

7.4 The Elementary Beam Theory

MECHANICS OF MATERIALS REVIEW

Are You Ready? Find Area in the Coordinate Plane

MTE 119 STATICS LECTURE MATERIALS FINAL REVIEW PAGE NAME & ID DATE. Example Problem F.1: (Beer & Johnston Example 9-11)

3.032 Problem Set 2 Solutions Fall 2007 Due: Start of Lecture,

PROBLEM 8.3. S F = 0: N -(250 lb)cos 30 -(50 lb)sin 30 = SOLUTION

BEAM DEFLECTION THE ELASTIC CURVE

MECHANICS OF SOLIDS - BEAMS TUTORIAL 1 STRESSES IN BEAMS DUE TO BENDING

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

Errata Sheet for S. D. Rajan, Introduction to Structural Analysis & Design (1 st Edition) John Wiley & Sons Publication

Design of Steel Structures Prof. S.R.Satish Kumar and Prof. A.R.Santha Kumar

Sub. Code:

7 TRANSVERSE SHEAR transverse shear stress longitudinal shear stresses

Transcription:

RCH 1 Note Set 9. S015abn Moments of nertia Notation: b d d d h c Jo O = name for area = name for a (base) width = calculus smbol for differentiation = name for a difference = name for a depth = difference in the direction between an area centroid ( ) and the centroid of the composite shape ( ˆ ) = difference in the direction between an area centroid ( ) and the centroid of the composite shape ( ŷ ) = name for a height = moment of inertia about the centroid = moment of inertia of a component about the centroid = moment of inertia with respect to an -ais = moment of inertia with respect to a -ais = polar moment of inertia, as is J = name for reference origin ro r r tf tw ˆ ŷ P L = polar radius of gration = radius of gration with respect to an -ais = radius of gration with respect to a -ais = thickness of a flange = thickness of web of wide flange = horizontal distance = the distance in the direction from a reference ais to the centroid of a shape = the distance in the direction from a reference ais to the centroid of a composite shape = vertical distance = the distance in the direction from a reference ais to the centroid of a shape = the distance in the direction from a reference ais to the centroid of a composite shape = plate smbol = smbol for integration = summation smbol The cross section shape and how it resists bending and twisting is important to understanding beam and column behavior. Definition: Moment of nertia; the second area moment d d We can define a single integral using a narrow strip: d = d for,, strip is parallel to for, strip is parallel to * can be negative if the area is negative (a hole or subtraction). el d shape that has area at a greater distance awa from an ais through its centroid will have a larger value of. 1

RCH 1 Note Set 9. S015abn Just like for center of gravit of an area, the moment of inertia can be determined with respect to an reference ais. Definition: Polar Moment of nertia; the second area moment using polar coordinate aes J o J o r d d d Definition: Radius of Gration; the distance from the moment of inertia ais for an area at which the entire area could be considered as being concentrated at. r r r radius of gration in radius of gration in J o ro polar radius of gration, and ro = r + r pole o r The Parallel-is Theorem The moment of inertia of an area with respect to an ais not through its centroid is equal to the moment of inertia of that area with respect to its own parallel centroidal ais plus the product of the area and the square of the distance between the two aes. d d d -d d d d d B d d B ais through centroid at a distance d awa from the other ais ais to find moment of inertia about but d 0, because the centroid is on this ais, resulting in: c d (tet notation) or d where c (or )is the moment of inertia about the centroid of the area about an ais and d is the distance between the parallel aes

RCH 1 Note Set 9. S015abn Similarl d Moment of inertia about a ais J o J c d Polar moment of nertia ro rc d Polar radius of gration r Radius of gration r d * can be negative again if the area is negative (a hole or subtraction). ** f is not given in a chart, but are: YOU MUST CLCULTE & WTH d Composite reas: where is the moment of inertia about the centroid of the component area d Basic Steps d is the distance from the centroid of the component area to the centroid of the composite area (ie. d = - ) ŷ 1. Draw a reference origin.. Divide the area into basic shapes. Label the basic shapes (components) 4. Draw a table with headers of Component, rea,,,,,, d, d,, d, d 5. Fill in the table values needed to calculate ˆ and 6. Fill in the rest of the table values. ŷ for the composite 7. Sum the moment of inertia ( s) and d columns and add together.

RCH 1 Note Set 9. S015abn Geometric Properties of reas about bottom left rea = bh = b/ = h/ Triangle b 1 ' 6b h rea = bh b h rea = r = 0 = 0 d 4 = = 0.1098r 4 4 r 8 = 0.0549r 4 = 0.0549r 4 rea = r d = 0 rea = r d 4 = 4r = 4r 8 = 4r 16 rea = = 0 = 0 ab = 16ah 175 = 4a h 15 rea = = 0 4ah = h 5 = 7ah 100 rea = ah = a h 80 = a = h 4 10 4

RCH 1 Note Set 9. S015abn Eample 1 (pg 57) 1 ˆ.05" Find the moments of inertia ( ˆ =.05, ŷ = 1.05 ). 1 ˆ 1.05" Eample (pg 5) 5

RCH 1 Note Set 9. S015abn Eample Determine the moments of inertia about the centroid of the shape. Solution: There is no reference origin suggested in figure (a), so the bottom left corner is good. n figure (b) area will be a complete rectangle, while areas C and are "holes" with negative area and negative moment of inertias. o rea = 00 mm 100 mm = 0000 mm = (00 mm)(100 mm) /1 = 16.667 10 6 mm 4 = (00 mm) (100 mm)/1 = 66.667 10 6 mm 4 rea B = -(0 mm) = -87.4 mm = = - (0 mm) 4 /4 = -0.66 10 6 mm 4 rea C = -1/(50 mm) = 97.0 mm = - (50 mm) 4 /8 = -.454 10 6 mm 4 = -0.1098(50 mm) 4 = -0.686 10 6 mm 4 rea D = 100 mm 00 mm 1/ = 10000 mm = (00 mm)(100 mm) /6 = 5.556 10 6 mm 4 = (00 mm) (100 mm)/6 =. 10 6 mm 4 shape (mm ) (mm) (mm ) (mm) (mm ) 0000 100 000000 50 1000000 B -87.4 150-44115 50-1417 C -96.99 1.066-8. 50-19650 D 10000 66.66667 666666.7 1. 1 45.58 15918 199561 15918mm ˆ 45.58mm 199561 mm ˆ 45.58 mm 9. 9 mm 85. 8 mm shape (mm 4 ) d (mm) d (mm 4 ) (mm 4 ) d (mm) d (mm 4 ) 16666667 5.8 56800 66666667-7.1 100800 B -6617 5.8-6751.7-6617 -57.1-91859.09 C -45469 5.8-50988.51-68650 71.6794-0176595. D 5555556-47.5 594177.8 6. 6881876.09 1911680 95707.5 87566466-1505111.9 So, = 1911680 + 95707.5 = 58701918 = 58.7 10 6 mm 4 = 87566466 +-1505111. = 45705 = 66.1 10 6 mm 4 6

RCH 1 Note Set 9. S015abn Eample 4 (pg 58) 7

RCH 1 Note Set 9. S015abn Eample 5 (pg 49)*.8 lso determine the moment of inertia about both major centroidal aes. 0. shape (in ) (in) (in ) (in) (in ) channel 6.09 0 0.00 9.694 59.04 left plate 5 -.5-16.5 5.11 5.55 right plate 5.5 16.5 5.11 5.55 wide flange 4.71 0 0.00 0 0.00 0.80 0.00 110.14 0 in ˆ 0.8 in 110.14 in ˆ 0.8 in 0 in 5.95 in shape (in 4 ) d (in) d (in 4 ) (in 4 ) d (in) d (in 4 ) channel.880-4.99 117.849 19.000 0.000 0.000 left plate 41.667 0.185 0.171 0.104.50 5.81 right plate 41.667 0.185 0.171 0.104 -.50 5.81 wide flange.800 5.95 1.054 10.000 0.000 0.000 90.01 50.45.08 105.65 = 90.01 + 50.45 = 40.59 = 40. in 4 =.08 + 105.65 = 7.8 = 7.8 in 4 8