Find: KCE λc>1.50 E = 2.9 * 107 [lb/in2] AC, CE  W12x120 BC 

Slides:



Advertisements
Similar presentations
Copyright © 2010 Pearson Education South Asia Pte Ltd
Advertisements

Beams Stephen Krone, DSc, PE University of Toledo.
REVIEW OF STEEL DESIGN KNOWLEDGE BASE REQUIRED: STRENGTH OF MATERIALS
Beam-Columns.
Rigid-Frame Structures
ME221Lecture #311 ME 221 Statics Lecture #31 Sections 6.6 – 6.7.
EGR 280 Mechanics 4 – Analysis of Structures Trusses.
BEARING OR CRUSHING Bearing Stresses (Compression Perpendicular to the Grain) Allowable stresses for compression perpendicular to the grain are available.
C-23 The effective length factor (K) was introduced in page (C-7) for six ideal conditions, these are not encountered in practical field conditions. LRFD.
Approximate Analysis of Statically Indeterminate Structures
Combined Bending & Axial Forces (BEAM – COLUMNS)
Combined Bending & Axial Forces (BEAM – COLUMNS)
LRFD-Steel Design 1.
Beam Analysis Civil Engineering and Architecture
Engineering Mechanics: Statics
EXAMPLE 4 Use properties of equality LOGO You are designing a logo to sell daffodils. Use the information given. Determine whether m EBA = m DBC. SOLUTION.
Beam Analysis Civil Engineering and Architecture
LRFD- Steel Design Dr. Ali I. Tayeh First Semester Dr. Ali I. Tayeh First Semester.
1.
Statics Solution Video By: William Rice, Mark Vogan, Jack Snell, and Robert Moss MAE /4/2010.
Engineering Mechanics: Statics
Engineering Mechanics: Statics
7.3 Relations between Distributed Load, Shear and Moment
Step 1: Graph the points. You can extend the graph if needed.
Second Order Analysis In the previous classes we looked at a method that determines the load corresponding to a state of bifurcation equilibrium of a perfect.
By: Adam Linnabery. The quadratic formula is –b+or-√b 2 -4ac 2a an example of how it is used: X 2 -4x-12=0 the coefficient of x 2 is 1 therefore the value.
STEEL DESIGN KNOWLEDGE BASE REQUIRED: STRENGTH OF MATERIALS STEEL DESIGN REVIEW OF TIMBER DESIGN BEARING PROBLEM TIMBER DESIGN SOIL MECHANICS REVIEW OF.
N.W.F.P. University of Engineering and Technology Peshawar 1 By: Prof Dr. Akhtar Naeem Khan Lecture 09: Compression Members.
Structures Agenda: Forces & Architectural Form - review
Collinearity, Betweeness, and Assumptions
Solid Mechanics Course No. ME213.
CE # 498 بســــم الله الرحمن الرحيـــم
Buckling & Stability Critical Load
Columns and Other Compression Members
Introduction to Structural Member Properties
Effective Length Coefficients
13.3 Columns with Various Types of Supports:
Factoring Special Cases
Vietnam Institute for Building Science and Technology (IBST)
3x 2x -5 x + 11 (4x + 7)° 90° (8x - 1)°.
Buckling & Stability Critical Load
Find: The Lightest I Beam
Find: Lightest Angled Beam
Find: QBE gal min 2, A F B Pipe AB BC CD DE EF FA BE C
Introduction to Structural Member Properties
Beam-Columns.
Chapter Objectives Chapter Outline To find forces in Truss by
Find: Fcr [lb/in2] Fcr E = 2.9 * 107 [lb/in2] fy = 36,000 [lb/in2]
Find: FCD [kN] 25.6 (tension) 25.6 (compression) 26.3 (tension)
REVIEW OF STEEL DESIGN KNOWLEDGE BASE REQUIRED: STRENGTH OF MATERIALS
Calculating Truss Forces
Find: Lightest I Beam fy=50,000 [lb/in2] unfactored axial
PLASTIC ANALYSIS OF STRUCTURES
Find: λc P P 1[in] fixed y 8 [in] A A’ 14[in] x 1[in] L z z fixed L/2
Find: φcPn [lb] column in compression E = 2.9 * 107 [lb/in2]
Idealized Model of Column Buckling in Frame Column Buckling in Frame
ANALYSIS OF STRUCTURES
Built-In Column The critical load for other column can be expressed in terms of the critical buckling load for a pin-ended column. From symmetry conditions.
ANALYSIS OF STRUCTURES
Find: co [ft/s] ua = 20 [mi/hr] d = 2 [hr] duration F = 15 [mi]
ANALYSIS OF STRUCTURES
Find: AreaABCD [acres]
Mechanics of Materials Engr 350 – Lecture 38 Columns
Find: AreaABCD [ft2] C 27,800 30,500 B 33,200 36,000 N A D set up
Find: M [k*ft] at L/2 A B w 5 w=2 [k/ft] 8 21 L=10 [ft] 33 L
Chapter Objectives Determine the forces in the members of a truss using the method of joints and the method of sections Analyze forces acting on the members.
Vector Equations Trig 6.12 Obj: Find the vector equation parallel to a given vector and through a given point.
Engineering Mechanics: Statics
KNOWLEDGE BASE REQUIRED:
Introduction to Structural Member Properties
Presentation transcript:

Find: KCE λc>1.50 E = 2.9 * 107 [lb/in2] AC, CE  W12x120 BC  unbraced CD  W24x68 A 12 [ft] A) 0.83 B) 0.95 C) 1.30 D) 1.85 B C D Find the effective length factor, K, for column C E. [pause] In this problem, --- 15 [ft] E 20 [ft] 18 [ft]

Find: KCE λc>1.50 E = 2.9 * 107 [lb/in2] AC, CE  W12x120 BC  unbraced CD  W24x68 A 12 [ft] A) 0.83 B) 0.95 C) 1.30 D) 1.85 B C D an unbraced, 2-story structure is connected with pin connections. The lengths of the --- 15 [ft] E 20 [ft] 18 [ft]

Find: KCE λc>1.50 E = 2.9 * 107 [lb/in2] AC, CE  W12x120 BC  unbraced CD  W24x68 A 12 [ft] A) 0.83 B) 0.95 C) 1.30 D) 1.85 B C D columns and girders are provided, and the specific I beams are specified for --- 15 [ft] E 20 [ft] 18 [ft]

Find: KCE λc>1.50 E = 2.9 * 107 [lb/in2] AC, CE  W12x120 BC  unbraced CD  W24x68 A 12 [ft] A) 0.83 B) 0.95 C) 1.30 D) 1.85 B C D 4 of the members. We also know, the slenderness parameter, --- 15 [ft] E 20 [ft] 18 [ft]

Find: KCE λc>1.50 E = 2.9 * 107 [lb/in2] AC, CE  W12x120 BC  unbraced CD  W24x68 A 12 [ft] A) 0.83 B) 0.95 C) 1.30 D) 1.85 B C D lambda c, is greater than 1.50. [pause] The effective length factor for a column, --- 15 [ft] E 20 [ft] 18 [ft]

Find: KCE λc>1.50 KCE = f (GC, GE) E = 2.9 * 107 [lb/in2] AC, CE  W12x120 unbraced BC  W24x55 A CD  W24x68 12 [ft] A) 0.83 B) 0.95 C) 1.30 D) 1.85 B C D as part of a structural frame, is a function of ---- 15 [ft] E 20 [ft] 18 [ft]

Find: KCE λc>1.50 KCE = f (GC, GE) E = 2.9 * 107 [lb/in2] end condition unbraced coefficient A 12 [ft] A) 0.83 B) 0.95 C) 1.30 D) 1.85 B C D the end condition coefficients, at the 2 ends, of the column. So for column C E, --- 15 [ft] E 20 [ft] 18 [ft]

Find: KCE λc>1.50 KCE = f (GC, GE) E = 2.9 * 107 [lb/in2] end condition unbraced coefficient A 12 [ft] A) 0.83 B) 0.95 C) 1.30 D) 1.85 B C D we’ll focus on joints C and E. [pause] Once we know the 2 --- 15 [ft] E 20 [ft] 18 [ft]

Find: KCE λc>1.50 KCE = f (GC, GE) E = 2.9 * 107 [lb/in2] end condition unbraced coefficient A 12 [ft] A) 0.83 B) 0.95 C) 1.30 D) 1.85 B C D end condition coefficients, we’ll use an alignment chart --- 15 [ft] E 20 [ft] 18 [ft]

Find: KCE λc>1.50 KCE = f (GC, GE) E = 2.9 * 107 [lb/in2] end condition unbraced coefficient A GE B C D GC to find the effective length factor for the column, ---- E Gtop K Gbottom 20 [ft] 18 [ft]

Find: KCE λc>1.50 KCE = f (GC, GE) E = 2.9 * 107 [lb/in2] end condition unbraced coefficient A KCE GE B C D GC K. [pause] The end condition coefficient, G, equals, --- E Gtop K Gbottom 20 [ft] 18 [ft]

Find: KCE Σ Ec * Ic / Lc Σ Eg * Ig / Lg E = 2.9 * 107 [lb/in2] KCE = f (GC, GE) Σ Ec * Ic / Lc G= Σ Eg * Ig / Lg A KCE GE B C D GC the sum of the E I over L, for the adjoining column members, divided by, --- E Gtop K Gbottom 20 [ft] 18 [ft]

Find: KCE Σ Ec * Ic / Lc Σ Eg * Ig / Lg E = 2.9 * 107 [lb/in2] KCE = f (GC, GE) Σ Ec * Ic / Lc adjoining columns G= Σ Eg * Ig / Lg adjoining girders A KCE GE B C D GC the sum of the E I over L, for the adjoining girders. E Gtop K Gbottom 20 [ft] 18 [ft]

Find: KCE Σ Ec * Ic / Lc Σ Eg * Ig / Lg E = 2.9 * 107 [lb/in2] KCE = f (GC, GE) Σ Ec * Ic / Lc adjoining columns GC= Σ Eg * Ig / Lg adjoining girders A KCE GE B C D GC For joint C, the column members will be --- E Gtop K Gbottom 20 [ft] 18 [ft]

Find: KCE Σ Ec * Ic / Lc Σ Eg * Ig / Lg E = 2.9 * 107 [lb/in2] KCE = f (GC, GE) Σ Ec * Ic / Lc adjoining columns GC= Σ Eg * Ig / Lg adjoining girders A KCE GE B C D GC A C and C E, and the girder members will be --- E Gtop K Gbottom 20 [ft] 18 [ft]

Find: KCE Σ Ec * Ic / Lc Σ Eg * Ig / Lg E = 2.9 * 107 [lb/in2] KCE = f (GC, GE) Σ Ec * Ic / Lc adjoining columns GC= Σ Eg * Ig / Lg adjoining girders A B C D KCE GE GC B C, and C D. [pause] From the problem statement, --- E Gtop K Gbottom 20 [ft] 18 [ft]

Find: KCE Σ Ec * Ic / Lc Σ Eg * Ig / Lg E = 2.9 * 107 [lb/in2] KCE = f (GC, GE) Σ Ec * Ic / Lc adjoining columns GC= Σ Eg * Ig / Lg adjoining girders A AC, CE  W12x120 B C D we know the specific I beams corresponding to these adjoining members. And we can --- CD  W24x68 E BC  W24x55 20 [ft] 18 [ft]

Find: KCE Σ Ec * Ic / Lc Σ Eg * Ig / Lg E = 2.9 * 107 [lb/in2] KCE = f (GC, GE) Σ Ec * Ic / Lc adjoining columns GC= Σ Eg * Ig / Lg adjoining girders A AC, CE  W12x120 B C D I=1,070 [in4] look up their corresponding area moment of inertia values, in the strong direction. [pause] Next we’ll write out the --- CD  W24x68 I=1,830 [in4] E BC  W24x55 20 [ft] 18 [ft] I=1,350 [in4]

Find: KCE E = 2.9 * 107 [lb/in2] KCE = f (GC, GE) joint C Ec*IAC/LAC + Ec*ICE/LCE GC= Eg*IBC/LBC + Eg*ICD/LCD A AC, CE  W12x120 B C D I=1,070 [in4] the equation for G, specific to joint C. Unless otherwise noted, we’ll assume --- CD  W24x68 I=1,830 [in4] E BC  W24x55 20 [ft] 18 [ft] I=1,350 [in4]

Find: KCE E = 2.9 * 107 [lb/in2] KCE = f (GC, GE) joint C Ec*IAC/LAC + Ec*ICE/LCE GC= Eg*IBC/LBC + Eg*ICD/LCD A AC, CE  W12x120 B C D I=1,070 [in4] the modulus of elasticity is constant for all members, therefore, --- CD  W24x68 I=1,830 [in4] E BC  W24x55 20 [ft] 18 [ft] I=1,350 [in4]

Find: KCE E = 2.9 * 107 [lb/in2] KCE = f (GC, GE) joint C Ec*IAC/LAC + Ec*ICE/LCE GC= Eg*IBC/LBC + Eg*ICD/LCD A AC, CE  W12x120 B C D I=1,070 [in4] it cancels out of the equation, and we’ll revise our equation for --- CD  W24x68 I=1,830 [in4] E BC  W24x55 20 [ft] 18 [ft] I=1,350 [in4]

Find: KCE = E = 2.9 * 107 [lb/in2] KCE = f (GC, GE) Ec*IAC/LAC + Ec*ICE/LCE IAC/LAC+ICE/LCE GC= = Eg*IBC/LBC + Eg*ICD/LCD IBC/LBC+ICD/LCD A AC, CE  W12x120 B C D I=1,070 [in4] the end condition coefficient, at Joint C. Next, we’ll plug in --- CD  W24x68 I=1,830 [in4] E BC  W24x55 20 [ft] 18 [ft] I=1,350 [in4]

Find: KCE = E = 2.9 * 107 [lb/in2] KCE = f (GC, GE) Ec*IAC/LAC + Ec*ICE/LCE IAC/LAC+ICE/LCE GC= = Eg*IBC/LBC + Eg*ICD/LCD IBC/LBC+ICD/LCD A AC, CE  W12x120 B C D I=1,070 [in4] the area moment of inertia terms, as well as the length terms, --- CD  W24x68 I=1,830 [in4] E BC  W24x55 20 [ft] 18 [ft] I=1,350 [in4]

Find: KCE = E = 2.9 * 107 [lb/in2] KCE = f (GC, GE) Ec*IAC/LAC + Ec*ICE/LCE IAC/LAC+ICE/LCE GC= = Eg*IBC/LBC + Eg*ICD/LCD IBC/LBC+ICD/LCD A AC,CE 12 [ft] B C D I=1,070 [in4] and our value of G, at joint C, --- CD 15 [ft] I=1,830 [in4] E BC 20 [ft] 18 [ft] I=1,350 [in4]

Find: KCE = GC=0.95 KCE = f (GC, GE) Ec*IAC/LAC + Ec*ICE/LCE IAC/LAC+ICE/LCE GC= = Eg*IBC/LBC + Eg*ICD/LCD IBC/LBC+ICD/LCD A AC,CE 12 [ft] B C D I=1,070 [in4] equals, 0.95. [pause] For Joint E, --- CD 15 [ft] I=1,830 [in4] E BC 20 [ft] 18 [ft] I=1,350 [in4]

Find: KCE = GC=0.95 KCE = f (GC, GE) Ec*IAC/LAC + Ec*ICE/LCE IAC/LAC+ICE/LCE GC= = Eg*IBC/LBC + Eg*ICD/LCD IBC/LBC+ICD/LCD A AC,CE 12 [ft] B C D I=1,070 [in4] since pin connections do not resist moments, pinned ends are assigned --- CD 15 [ft] I=1,830 [in4] E BC 20 [ft] 18 [ft] I=1,350 [in4]

Find: KCE = GC=0.95 KCE = f (GC, GE) Ec*IAC/LAC + Ec*ICE/LCE IAC/LAC+ICE/LCE GC= = Eg*IBC/LBC + Eg*ICD/LCD IBC/LBC+ICD/LCD A AC,CE 12 [ft] B C D I=1,070 [in4] a value of 10, for their end condition coefficient. [pause] Returning to the --- CD GE=10 15 [ft] I=1,830 [in4] E BC 20 [ft] 18 [ft] I=1,350 [in4]

Find: KCE = GC=0.95 KCE = f (GC, GE) Ec*IAC/LAC + Ec*ICE/LCE IAC/LAC+ICE/LCE GC= = Eg*IBC/LBC + Eg*ICD/LCD IBC/LBC+ICD/LCD A B C D alignment chart. We’ll mark the values for G C and ---- GE=10 E Gtop K Gbottom 20 [ft] 18 [ft]

Find: KCE = GC=0.95 KCE = f (GC, GE) Ec*IAC/LAC + Ec*ICE/LCE IAC/LAC+ICE/LCE GC= = Eg*IBC/LBC + Eg*ICD/LCD IBC/LBC+ICD/LCD A GE B C D GC G E. [pause] Drawing a straight line between these points helps us --- GE=10 E Gtop K Gbottom 20 [ft] 18 [ft]

Find: KCE = GC=0.95 KCE = f (GC, GE) Ec*IAC/LAC + Ec*ICE/LCE IAC/LAC+ICE/LCE GC= = Eg*IBC/LBC + Eg*ICD/LCD IBC/LBC+ICD/LCD A GE B C D GC identify the effective length factor for column C E, which equals, --- GE=10 KCE E Gtop K Gbottom 20 [ft] 18 [ft]

Find: KCE = GC=0.95 KCE = f (GC, GE) Ec*IAC/LAC + Ec*ICE/LCE IAC/LAC+ICE/LCE GC= = Eg*IBC/LBC + Eg*ICD/LCD IBC/LBC+ICD/LCD A GE B C D GC 1.85. [pause] GE=10 KCE=1.85 E Gtop K Gbottom 20 [ft] 18 [ft]

Find: KCE = GC=0.95 KCE = f (GC, GE) Ec*IAC/LAC + Ec*ICE/LCE IAC/LAC+ICE/LCE GC= = Eg*IBC/LBC + Eg*ICD/LCD IBC/LBC+ICD/LCD A) 0.83 B) 0.95 C) 1.30 D) 1.85 GE GC When looking back at the possible solutions, --- KCE=1.85 Gtop K Gbottom

Find: KCE = GC=0.95 KCE = f (GC, GE) Ec*IAC/LAC + Ec*ICE/LCE IAC/LAC+ICE/LCE GC= = Eg*IBC/LBC + Eg*ICD/LCD IBC/LBC+ICD/LCD A) 0.83 B) 0.95 C) 1.30 D) 1.85 GE GC the answer is D. KCE=1.85 answerD Gtop K Gbottom