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    Structural Analysis-I

    Dr. Anis Shatnawi

    Second Semester

    2013-2014

    Lecture 1

    Structural Analysis

    Introduction tothe Course

    2

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    Intro 3

    Introduction-Contents

    Previous Structures Courses Stress Equations

    Static Determinacy and Indeterminacy

    This Course

    Types of Structures

    Getting Feedback

    Loads

    Units and Accuracy

    Sign Conventions

    Principle of Superposition

    Intro 4

     A structure refers to a system of connected

     parts used to support a load.

    Important examples related to civil engineering

    include buildings, bridges, and towers; and in otherbranches of engineering, ship and aircraft frames,

    tanks, pressure vessels, mechanical systems, and

    electrical supporting structures are important.

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    Intro 5

    We examine Structures in this classBridge

    RainbowBridge inFolsom

    Intro 6

    We examine Structures in this classAnother Bridge

    Vancouver, B.C.

    •Note it is composed of several smallerstructures, called substructures.

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    Intro 7

    We examine Structures in this classAnother Bridge-Closer View

    Quick

    view of

    Tacoma

    Narrows

    Bridge

    Note it is composed of several substructures.

    How many different substructures can youidentify?

    Suspension Cables

    Tension Cables

    Stiffening Truss

    Support Frames

    Roadway/Beams

     Any Others?

    Intro 8

    We examine Structures in this classAnother Bridge-End View

    Tower Support Frames

    Foundation

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    Intro 9

    Very Big BridgeLongest single arch bridge in the country

    New River Gorge- West Virginia

    I nt ro 1 0

    Very Big Bridge

    Steel bridge

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    I nt ro 11

    Very Big Bridge Note how three-dimensional the

    bridge is!

    I nt ro 1 2

    What is this class?

    StaticsDeals with equilibrium of rigid bodies.Structures did NOT deform.

    Mechanics of MaterialsLooked at what goes on inside a structure 

    when loads are applied. Structures deform,

    that is, they change shape.

    You have had two previous courses in structures:

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    I nt ro 1 3

    Statics

    Statics is Equilibrium:

    •These are vector equations.

    •In 2D, there are 2 force and 1 momentequations, for a total of 3 equations.

    •In 3D there are 3 force and 3 momentequations, for a total of 6 equations.

     

    F=0

     

    M=0

    What did you do in Statics?

    I nt ro 1 4

    Statics

    Equilibrium:

    Equilibrium is very important for thiscourse.

    WARNING: Most errors you make inthis course will be errors in applying

    equilibrium.

     

    F=0

     

    M=0

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    I nt ro 1 5

    Free Body Diagrams (FBD)

    The concept of a FBD is very important.

     A FBD of the entire structure will show allforces acting on it. You replace the supports

    with the reactive forces that are supplied by the

    supports.

    I nt ro 1 6

    Free Body Diagrams (FBD)

    The concept of a FBD is very important.

     A FBD can be only a portion of the structureobtained by taking a section at one or more

    points.

     A FBD of the entire structure will show allforces acting on it. You replace the supports

    with the reactive forces that are supplied by the

    supports.

    You must show all forces on the FBD.When a section is taken you must include

    all internal forces acting at the section.

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    I nt ro 1 7

    External and Internal Forces

    There are two basic types of forces,External and Internal:

    External forces are those that act on the FBD.Loads and reactions are examples.

    I nt ro 1 8

    External and Internal Forces

    There are two basic types of forces,External and Internal:

    External forces are those that act on the FBD.Loads and reactions are examples.

    Internal forces exist within the structure andare necessary to hold the structure together. Axial forces, shear forces and bendingmoments are examples.

    Internal forces always occur in pairs, sincetaking a section will produce two FBD’s andeach FBD must have the internal force actingon it.

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    I nt ro 1 9

    Reactions at Supports

    In 2 dimensions, there are basicallythree types of supports.

    R

    y

    Roller -has only 1 force reaction to prevent

    translation in 1 direction. The reaction can

    act up or down.R

    xR

    y

    Pin -supplies 2 force reactions to prevent

    translation in 2 directions.

    Fixed-provides the 2 force reactions likethe pin but also prevents rotation by

    supplying a moment reaction.

    Note that the

    reactions arealways shown

    in the positive

    directions.

    R

    x R

    y

    MR

    I nt ro 2 0

    Mechanics of Materials

    In this course we allowed the structures todeform, i.e. change in shape.

    Strain is the quantitative measure of thisdeformation.

    Stress is related to strain through Hooke’s law.

    You learned to calculate stresses, strains, anddisplacements of structures in mechanics.

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    I nt ro 2 1

    Displacement and Deformation

    Displacement is the movement from onelocation to another.

    Deformation means a change in shape.

    You can have one without the other.

    They usually occur together.

    Can you think of examples of them

    occurring separately and together?

    I nt ro 2 2

    Stress Equations from Mechanics

    These equations for stress are justfine. We really cannot improveupon them.

    J

    Tr

    Ib

    VQ

    I

    My

    A

    N

    T

    V

    M

    ax

     

    How about A; I; and J? Or  y or r? Q? Or N; M; V; T?

    Which quantities in theseequations are most difficult to find?

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    I nt ro 2 3

    Statically Determinate Structures

     A structure is Statically Determinate (SD) ifyou can calculate all reactions and internalforces just using the equations of statics, i.e.equations of equilibrium.

    This means that you must have the samenumber of unknowns as you have equationsof equilibrium.

    Number of unknowns=Number of equilibrium equations All problems we examined in Statics and most

    in Mechanics were statically determinate.

    I nt ro 2 4

    Statically Indeterminate Structures

     A structure is Statically Indeterminate(SI) if you cannot calculate all reactions andinternal forces just using the equations ofstatics, i.e. equations of equilibrium.

    This means that you have more unknownsthan you have equations of equilibrium.

    You solved a few SI problems in yourMechanics class.

    Number of unknowns>Number of equilibrium equations

    But not many!

    In this class we solve SI problems!

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    I nt ro 2 5

    Example 1

    P

    This beam has 2 unknown reactions, R A and RB.

    RA RB

    In a beam, there are assumed to be no hor izontalforces and therefore we show no horizontalreactions on a beam.

    There are 2 equilibr ium equations instead of theusual 3 because the FX=0 gives us no usefulinformation since there are no horizontal forces.

    2 equations to solve for the 2 unknown reactionsmeans this problem is Statically Determinate (SD).Number of equations =Number of unknowns

    I nt ro 2 6

    Example 2

    This beam has 3 unknown reactions,R A, RB, and RC.

    PP

    RA RB RC

    There are still only 2 equilibrium equations.

    2 equations to solve for the 3 unknownreactions means it is StaticallyIndeterminate (SI).

    Why no R AX?

    Number of equations < Number of unknowns

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    I nt ro 2 7

    Example 2

    This beam has 3 unknown reactions,R A, RB, and RC.

    PP

    RA RB RC

    There are still only 2 equilibrium equations.

    2 equations to solve for the 3 unknownreactions means it is StaticallyIndeterminate (SI).

    Why no R AX?

    Since there is 1 more unknown thanequations, we say it is SI 1.

    I nt ro 2 8

    Example 3

    This beam has 4 unknown reactions, R A, RB,RC, & M A.

    PP

    RB RCRA

    MA

    There are still only 2 equilibrium equations.

    2 equations to solve for the 4 unknownreactions means this problem is StaticallyIndeterminate (SI). equations < unknowns

    Since there are 2 more unknowns thanequations, we say it is SI 2.

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    I nt ro 2 9

    In the stress equations, the internal forces, Vand M for a beam, are the most difficult termsto evaluate if the structure is at all complicated.

    Main Goal in this Course

    For SI structures, evaluating these internalforces can be a formidable task.

    Finding these internal forces is the main

    goal of this course.

    I nt ro 3 0

    Once the internal forces are found, the stressequations from Mechanics can be used.

    Completing the Analysis

    Once the stresses are found, they are

    compared to the material strength to see ifthe structure is safe.

    In this class, we will usually stop after theinternal forces are found, but always rememberthat these next steps must always be performedto complete the analysis.

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    I nt ro 3 1

    The internal forces are best illustrated bydrawing the internal force diagrams.

    Internal Force Diagrams

    For beams, you are familiar with shear forceand bending moment diagrams.

    Trusses have only axial forces, no shear ormoment.

    For frames, we will have axial force, shearforce, and bending moment diagrams .

    I nt ro 3 2

    Sign Conventions

    We must be very careful with our signs.

    Remember that we always have two signconventions: equilibrium and beam.

    They are used for different purposes.

    They are not contradictory. They are complimentary.

    We always need to use the two conventionstogether.

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    I nt ro 3 3

      Fy=0: In this equation a force will be positiveif it acts upward, the positive direction of the y-axis.

      FX=0: In this equation a force will be positiveif it acts to the right, the positive direction ofthe x-axis.

    Equilibrium Sign Convention

    We use this for summing forces and moments ,e.g. to calculate reactions.

    x

    y

    z

    +

    +

    Positive horizontal force for equilibr ium

    Positive vertical force for equilibr ium

    I nt ro 3 4

    Equilibrium Sign Convention

     M=0. In this equation a moment will bepositive if it acts counterclockwise, (CCW),around the positive z-axis by the right handrule.

    We will maintain this consistent sign convention

    throughout the semester.

    Positive moment for

    applying equilibrium.

    x

    y

    z

    +

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    I nt ro 3 5

    Beam Sign Convention

    Axial Force:

    P   P

    P   P

    Compression is negative

    Tension is positive

    I nt ro 3 6

    Shear Force

    Take a section:

    +V makes the right FBD tends to rotate ClockWise

    +V

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    I nt ro 3 7

    Shear Force

    +V

    +V makes both FBD’s tend to rotate Clock Wise.

    I nt ro 3 8

    Shear Force

    -V causes a Counter Clock Wise (CCW)

    rotation of each Free Body Diagram (FBD)

    -V

    +V

    +V causes a Clock Wise (CW) rotation

    of each Free Body Diagram (FBD)

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    I nt ro 3 9

    Shear Force

    +V

    +V causes a Clock Wise (CW) rotation

    of each Free Body Diagram (FBD)

    -V

    -V causes a Counter Clock Wise (CCW)

    rotation of each Free Body Diagram (FBD)

    I nt ro 4 0

    Moment

    +M

    +M causes Compression to occur

    on the top of the beam

    Take a section:

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    I nt ro 4 1

    Moment

    +M

    +M causes Compression to occur

    on the top of the beam

    Notice the deformed shape.It holds water.

    Take a section:

    The deformed shape smiles at you

    I nt ro 4 2

    Moment

    -M causes Compression to occur

    on the bottom of the beam

    -M

    This deformed shape sheds water.

    +M

    +M causes Compression to occur

    on the top of the beam

    Smileyface

    Frowneyface

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    I nt ro 4 3

    Linear Problems

    Nearly all structures you have examined sofar are linear problems.

    For a linear problem, if you plot load vs. anyresult of that load (e.g. a reaction,displacement, internal force, etc.), you get astraight line.

    What is the only nonlinear problem you

    looked at in Mechanics? For linear problems, the Principle ofSuperposition always applies.

    I nt ro 4 4

    Principle of Superposition

    The Principle of Superposition says manythings :

    If you double the loads then you double anyresult of the loads.

    If you have several loads acting on thestructure, you can solve the problem for eachload separately and then add the results.

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    I nt ro 4 5

    Principle of Superposition-Loads

    For example:

    To solve this problem with both a concentratedload and a uniform load, we can solve the

    problem first for the load of P and then for the

    load of w0, and then add the results together.

    RBRA

    P w0

    L

    This beam has two loads: a concentrated load of

    P and a uniform load of w0.

    I nt ro 4 6

    Alwayscheck

    reactions!

     

    OKso 0P2

    P

    2

    PF:check

    2

    PR

    LR2

    LP0M

    2

    PR

    LR

    2

    LP0M

    y

    A

    AB

    B

    BA

     

     

     

     

    Principle of Superposition-Loads

    Look firstat the

    load of P

    RBRA

    P

    L

    2

    P

    2

    P

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    I nt ro 4 7

    Principle of Superposition-Loads

    Now look

    at the

    uniform

    load w0

    RBRA

    w0

    L

    2LwO

    2LwO

     

    0Lw2

    Lw

    2

    LwF:check

    2

    LwR

    LR2

    L

    Lw0M

    2

    LwR

    LR2

    LLw0M

    OOO

    y

    OA

    AOB

    OB

    BOA

     

     

     

     

     Always check

    reactions!

    I nt ro 4 8

    Principle of Superposition-Loads

    So, we just

    add together

    the solutions

    for these two

    simplerproblems to

    get the

    answer to the

    original

    problem

    RA RB

    P

    + RBRA

    w0

    RBRA

    Pw

    0

    =

    2

    P

    2

    P

    2LwO

    2LwO

    2Lw

    2

    PO

     

    2Lw

    2

    PO

     

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    I nt ro 4 9

    Principle of Superposition-Displacements

    It also works

    with

    displacements.

    Find those due

    to P, DP, and

    those due to

    w0

    , Dw

    , and

    add them

    together:

    D=DP+Dw.

    P w0

     

    D

    =

    w0

     

    Dw

    +

    P

     

    DP

    I nt ro 5 0

    Structural Analysis

    End ofIntroduction