Ch. 10 Design of Short Columns Subject to Axial Load and Bending

Similar documents
Purpose of reinforcement P/2 P/2 P/2 P/2

Chapter 6. Compression Reinforcement - Flexural Members

Interaction Diagram Dumbbell Concrete Shear Wall Unsymmetrical Boundary Elements

Slenderness Effects for Concrete Columns in Sway Frame - Moment Magnification Method

WRAP-AROUND GUSSET PLATES

TORSION By Prof. Ahmed Amer

Slenderness Effects for Concrete Columns in Sway Frame - Moment Magnification Method

Reinforced Concrete Design

twenty steel construction: columns & tension members ARCHITECTURAL STRUCTURES: FORM, BEHAVIOR, AND DESIGN DR. ANNE NICHOLS FALL 2018 lecture

Uniaxial Concrete Material Behavior

Software Verification

INFORMATION CONCERNING MATERIALS TO BE USED IN THE DESIGN

Case Study in Reinforced Concrete adapted from Simplified Design of Concrete Structures, James Ambrose, 7 th ed.

fib Model Code 2020 Shear and punching provisions, needs for improvements with respect to new and existing structures

Solid Mechanics Homework Answers

Designing Reinforced Concrete Rectangular Columns for Biaxial Bending

MECHANICS OF MATERIALS

This Technical Note describes how the program checks column capacity or designs reinforced concrete columns when the ACI code is selected.

Torsion. Torsion is a moment that twists/deforms a member about its longitudinal axis

Civil Engineering Design (1) Design of Reinforced Concrete Columns 2006/7

ε t increases from the compressioncontrolled Figure 9.15: Adjusted interaction diagram

1/2. E c Part a The solution is identical for grade 40 and grade 60 reinforcement. P s f c n A s lbf. The steel carries 13.3 percent of the load

The Design of Fiber Reinforced Polymers for Structural Strengthening An Overview of ACI 440 Guidelines. Sarah Witt Fyfe Company November 7, 2008

Strength of Materials

Dr. Hazim Dwairi 10/16/2008

Chapter 1 Introduction- Concept of Stress

Static Failure (pg 206)

Reinforced Concrete Design

and F NAME: ME rd Sample Final Exam PROBLEM 1 (25 points) Prob. 1 questions are all or nothing. PROBLEM 1A. (5 points)

Lecture-03 Design of Reinforced Concrete Members for Flexure and Axial Loads

Failure from static loading

B U I L D I N G D E S I G N

Wood Design. = theoretical allowed buckling stress

thirteen wood construction: column design ARCHITECTURAL STRUCTURES: FORM, BEHAVIOR, AND DESIGN DR. ANNE NICHOLS SUMMER 2017 lecture

Design of AAC floor slabs according to EN 12602

PROBLEM 7.1 SOLUTION. σ = 5.49 ksi. τ = ksi

Reinforced Concrete Design

Direct Design Method and Design Diagram. For Reinforced Concrete Columns and Shear walls

According to the Ratio of Height to Least Lateral Dimension: (ACI Code and ACI Code ) < 22, when member is braced against sideways.

A.1. Member capacities A.2. Limit analysis A.2.1. Tributary weight.. 7. A.2.2. Calculations. 7. A.3. Direct design 13

Observations in Shear Wall Strength in Tall Buildings. Presented by StructurePoint at ACI Spring 2012 Convention in Dallas, Texas

Reinforced Concrete Design

Strength of Material. Shear Strain. Dr. Attaullah Shah

Design of Reinforced Concrete Beam for Shear

Masonry Beams. Ultimate Limit States: Flexure and Shear

Compression Members Local Buckling and Section Classification

Mechanical Properties of Materials

Biaxial Analysis of General Shaped Base Plates

ACI Fall Convention 2010 Pittsburgh, PA ARGENTINA DOCUMENT

[5] Stress and Strain

Flexural Strength Design of RC Beams with Consideration of Strain Gradient Effect

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

[8] Bending and Shear Loading of Beams

4.MECHANICAL PROPERTIES OF MATERIALS

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.

Two-Way Flat Slab (Concrete Floor with Drop Panels) System Analysis and Design

Stress Transformation Equations: u = +135 (Fig. a) s x = 80 MPa s y = 0 t xy = 45 MPa. we obtain, cos u + t xy sin 2u. s x = s x + s y.

D : SOLID MECHANICS. Q. 1 Q. 9 carry one mark each. Q.1 Find the force (in kn) in the member BH of the truss shown.

CONNECTION DESIGN. Connections must be designed at the strength limit state

Please review the following statement: I certify that I have not given unauthorized aid nor have I received aid in the completion of this exam.

The casing is subjected to the following:

Stress Analysis Lecture 3 ME 276 Spring Dr./ Ahmed Mohamed Nagib Elmekawy

Software Verification

eighteen steel construction: column design ELEMENTS OF ARCHITECTURAL STRUCTURES: FORM, BEHAVIOR, AND DESIGN DR. ANNE NICHOLS SPRING 2019 lecture

Shear-Friction Strength of RC Walls with 550 MPa Bars

Reports RESEARCH REPORT RP00-3 RESEARCH REPORT RP01-1 OCTOBER REVISION 2006 REVISION

Virtual Work for Frames. Virtual Work for Frames. Virtual Work for Frames. Virtual Work for Frames. Virtual Work for Frames. Virtual Work for Frames

Design of Reinforced Concrete Beam for Shear

Introduction. ENCE 710 Design of Steel Structures IV. COMPOSITE STEEL-CONCRET CONSTRUCTION. Effective Width. Composite Action

twenty one concrete construction: materials & beams ELEMENTS OF ARCHITECTURAL STRUCTURES: FORM, BEHAVIOR, AND DESIGN DR. ANNE NICHOLS SPRING 2014

Problem d d d B C E D. 0.8d. Additional lecturebook examples 29 ME 323

MECHANICS OF MATERIALS. Prepared by Engr. John Paul Timola

ME 202 STRENGTH OF MATERIALS SPRING 2014 HOMEWORK 4 SOLUTIONS

Purpose of this Guide: To thoroughly prepare students for the exact types of problems that will be on Exam 3.

DESIGN OF BEAMS AND SHAFTS

Software Verification

Design of a Multi-Storied RC Building

Flexure: Behavior and Nominal Strength of Beam Sections

Lecture-04 Design of RC Members for Shear and Torsion

Example 4.1 [Uni-axial Column Design] Solution. Step 1- Material Step 2-Determine the normalized axial and bending moment value

Reinforced concrete structures II. 4.5 Column Design

BEAMS: SHEARING STRESS

Software Verification

MECHANICS OF MATERIALS Sample Problem 4.2

Column Design. Columns Axial Load and Bending

CONSULTING Engineering Calculation Sheet. Job Title Member Design - Reinforced Concrete Column BS8110

BEHAVIOR OF SQUARE CONCRETE-FILLED TUBULAR COLUMNS UNDER ECCENTRIC COMPRESSION WITH DOUBLE CURVATURE DEFLECTION

Rectangular Filament-Wound GFRP Tubes Filled with Concrete under Flexural. and Axial Loading: Analytical Modeling ABSTRACT

If the solution does not follow a logical thought process, it will be assumed in error.

Mechanics of Materials CIVL 3322 / MECH 3322

Mechanics of Solids. Mechanics Of Solids. Suraj kr. Ray Department of Civil Engineering

Torsion of Shafts Learning objectives

The science of elasticity

Bending and Shear in Beams

Samantha Ramirez, MSE. Stress. The intensity of the internal force acting on a specific plane (area) passing through a point. F 2


Chapter. Materials. 1.1 Notations Used in This Chapter

M. Vable Mechanics of Materials: Chapter 5. Torsion of Shafts

STRENGTH OF MATERIALS-I. Unit-1. Simple stresses and strains

Seismic Pushover Analysis Using AASHTO Guide Specifications for LRFD Seismic Bridge Design

Transcription:

Ch. 10 Design o Short Columns Subjet to Axial Load and Bending Axial Loading and Bending Development o Interation Diagram Column Design Using P-M Interation Diagram Shear in Columns Biaxial Bending Examples

Axial Load and Bending Equivalent

Development o Interation Diagrams

b u =0.003 0.85 M P h Y X As3, d3 As2, d2 As4, d4 s2 s3 s4 a s3 s2 s4 P F s4 C F s3 F s2 P n As1, d1 s1 Setion Strain Stress Equilibrium C F si 0.85 ab A si si where h a h M n C Fsi di 2 2 2 P-M interation urve an be onstruted by plotting (M n,p n ) or various s1 or. s1 si y F s1

Example 10.2: olumn setion 6 #29 bars 356 mm 64 mm 482 mm 64 mm 610 mm

Example 10.2: Strain Proile s 0.002 180 244 0.001475 a 0.85366 311. 1mm 1 0.003 s 302 366 0.002475 y 64 mm 180 mm 302 mm 64 mm 244 mm =366 mm 610 mm

Example 10.2: Fore Equilibrium s 0.001475 200000 295 MPa T s A s s 1935 29510 571kN 3 571 kn 2598 kn 801 kn 92 mm C 0.85 ab 0.85 27.6311.135610 2598 kn C s A 801kN 155 mm s s 1935 41410 3 3 P n M 149 mm 64 mm 241 mm 241 mm 64 mm C n C C h 2 s T s 305 mm 305 mm 2598 801 571 2828kN a F 2 si h d 2 si 311.1 2598305 571 241 801 241 10 2 718.9 kn m 3

Example 10.2: Tension Failure New Strain Proile s > y ( y ) 64 mm 610 mm

Example 10.2: P-M Interation Curve 6595 kn 2828 kn 718.9 kn-m 2245 kn 759 kn-m 403 kn-m 1602 kn

P-M Interation Diagram

P-M Interation Depending on Steel

P-M Curve with Strength Redution Fator (M n, P n ) (M n, P n )

st y st g n st y st g n A A A P A A A P 0.85 0.85 0.85 0.80 P-M Curve or Design

Modiiation o Strength Redution Fator

Column Design Using P-M Interation Diagrams Column design harts are nothing but P-M interation urves arranged in one o various ways The primary purpose o design harts is to make olumn design quik and easy without onstruting the P-M urve or every speii olumn It is important to keep the bar arrangement as lose as possible between the hart and reality

Estimation o Column Size Least dimension o retangular setion 200 mm Minimum diameter o irular setion 300 mm For tied olumns For spiral olumns A g 0. 45 Pu y A g 0. 55 Pu y

Example 10.3 The short 1420 in (356508 mm) tied olumn is to be used to support P D =125 k (556 kn), P L =140 k (623 kn), M D =75 k-t (102 kn-m) and M L =90 k-t (122 kn-m). I =4 ksi (27.6 MPa) and y =60 ksi (414 MPa), selet reinoring bars to be plaed in its end aes only using appropriate ACI olumn interation diagrams. (64 mm) Sine olumn design harts in SI units are not available, US ustomary units are used. (356 mm) (381) M u 1.2M D (508 mm) M u M n (64 mm) P u P e 1.2P n M P 1.6P 15 0.75 20 1.6M 234 0.65 36012 575.4 1.2125 1.6140 374 kips Pu 374 575.4 kips ( t y assumed ) 0.65 n n D L L 1.2 75 1.690 234 k t 360 k t 7.51in

Example 10.3 The short 1420 in (356508 mm) tied olumn is to be used to support P D =125 k (556 kn), P L =140 k (623 kn), M D =75 k-t (102 kn-m) and M L =90 k-t (122 kn-m). I =4 ksi (27.6 MPa) and y =60 ksi (414 MPa), selet reinoring bars to be plaed in its end aes only using appropriate ACI olumn interation diagrams. (356 mm) (64 mm) Pn 575.4 0.513 Ag 414 20 Pn e 575.47.51 0.193 Ag h 414 20 20 0.022 ( 0.7, Graph A3) 0.0185 ( 0.8, Graph A4) 0.0202 ( 0.75) (381) (508 mm) Ast bh 0.0202356508 3653mm 2 Use 6 #29( Ast, provided 3870 mm ) s Sine 0.55 1.0 t 0.002 y (64 mm) 0.65 O.K. 2

0.513 0.022 0.193

0.513 0.0185 0.193

Example 10.4 Design a short olumn or P u =600 kips (2670 kn), M u =125 k-t (170 kn-m), =4 ksi (27.6 MPa), y =60 ksi (414 MPa). Plae bars uniormly around all our aes. Determination o olumn setion, assuming 0.02 A g 0.45 Use 8#32( A u 0.454000 0.02 60000 1616in (256in 16 21.6 23/ 8 1 0.69 16 0.65assumed Pn A M A g n g Pu A 0.04 ( 0.6, 0.036 ( 0.7, ) 0 0.65, Graph A6) 0 0.65, Graph A7) 0.036 0.04 0.04 0.09 0.0364 ( 0.69) 0.1 2 2 A bh 0.0364 256 25.4 6012 mm st P g M u h A h g y st, provided 2 6552 mm 6001000 600 0.901 0.65 4 256 12512 0.141 0.65 4 25616 s s y y 2 ) 256in 2 64 279 mm 406 mm 64 64 mm 279 64 mm 406

0.901 0.04 0.141

0.901 0.036 0.141

Example 10.5 Selet reinoring bars or the short round spiral olumn i =4 ksi (27.6 MPa), y =60 ksi (414 MPa), P u =500 kips (2225 kn), M u =200 k-t (271 kn-m). 202580 mm 2 64 mm 381 mm 64 mm 508 mm Pu A M A 0.0175( 0.75 A u st g g Use 6#29( A Sine 500 0.531 0.75 4 314 200 12 0.127 h 0.75 4 314 20 15 0.75 20 0.0195( 0.7, 0.0155( 0.8, A s g y by interpolation) 0.0175 202580 3545mm st, provided 3870 mm 1.0,, 0.7 t s s y y y 0.45, Graph A11) 0.55, Graph A12) 2 ) 2

0.024 0.531 0.127

0.531 0.02 0.127

Example 10.7 Using the appropriate interation urves, determine the value o P n or the short tied olumn i e x =10 in (254 mm). Assume =4 ksi (26.7 MPa) and y =60 ksi (414 MPa). (76 mm) 3#32(2445 mm 2 ) 3#32(2445 mm 2 ) (305 mm) From Fig.10.15, Pn e A h g 0.24 is read P n 0.24 (356) (508) e (76 mm) A g h e 10 0.5 h 20 23.79 0.0316 12 20 14 0.7 20 0.24 412 20 20 10 460.8 kips

0.0316

Shear in Columns mm., units in positive in ompression and all load, atored axial where 6 1 0 3 1 tension, with axial ii) when aounting or lexure noted above or 8 4 (approximate) 6 1 14 1 ompression, with axial ii) 1 where (aounting or lexure) 0 3 7 120 (approximate) 6 1 load, without axial i) N N d b A N. V M d h N M M d b A N V M d V d b. d b M d V ρ V d b V u w g u u u u m w g u u u w w u u w w

Biaxial Bending

1 P P P P P ni where ni nx ny o 1 P Biaxial Bending Bresler Formula nx 1 P ny 1 P at an eentriity e at an eentriity e o the nominal axial load apaity o the setion when the load is plaed at a given eentriity along both axes the nominal axial load apaity o the setion when the load i splaed x the nominal axial load apaity o the setion when the load is plaed y the nominal axial load apaity o the setion when the load is plaed with a zero eentriity. It is usually taken as 0.85 A g A st y

Example 10.8 Determine the design apaity P ni o the short tied olumn subjeted to biaxial bending. Use =4 ksi (27.6 MPa), y =60 ksi (414 MPa), e x =16 in (406 mm) and e y =8 in (203 mm). (64 mm) Bending about X axis (8 #29) (64 mm) 254 (381 mm) (508) (635) (64 mm) 20 0.8 25 8 0.0213 15 25 e 16 0.64 h 25 Pn e 0.185 (Graph A8) A h P nx g 0.185 415 25 25 16 434 kips

e/h=0.64 0.0213 0.185

Example 10.8 Determine the design apaity P ni o the short tied olumn subjeted to biaxial bending. Use =4 ksi (27.6 MPa), y =60 ksi (414 MPa), e x =16 in (406 mm) and e y =8 in (203 mm). (64 mm) (8 #29) (64 mm) 254 (381 mm) (508) (635) (64 mm) Bending about Y axis 10 0.67 15 8 0.0213 15 25 e 8 0.53 h 15 Pn e 0.161 (Graph A6 and A7) Ag h 0.161 415 2515 Pny 452.3kips 8

e/h=0.53 0.0213 0.159

e/h=0.53 0.0213 0.177

(8 #29) (64 mm) Example 10.8 Determine the design apaity P ni o the short tied olumn subjeted to biaxial bending. Use =4 ksi (27.6 MPa), y =60 ksi (414 MPa), e x =16 in (406 mm) and e y =8 in (203 mm). (64 mm) 254 (381 mm) (508) (635) (64 mm) Axial loading apaity or M P 0.85 o Ag y Ast 0.85 415 25 608 1755 kips Using Bresler's ormula 1 1 1 1 Pni Pnx Pny Po 1 1 1 434 452.3 1755 P 253.5kips ni 0