CE 201-A4 p2_l18_l28

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    CE 201 - STATICSDr. Mustafa Y. Al-MandilDepartment of

    Civil Engineering

    LECTURE

    18 134

    EQUILIBRIUM OF RIGHD BODY

    It is necessary and sufficient for the equilibrium of rigid body that the resultant

    of all forces acting on the body is zero and that the resultant of all moments

    taken about any point inside or outside the body is zero.

    0~

    F~ 0

    ~M~

    0

    00

    z

    y

    x

    M

    MM

    Ox

    FR

    MR

    MC

    MF

    O

    MC

    &

    0

    00

    z

    y

    x

    F

    FF ...

    ...

    ...

    ...

    ...

    ...

    1F~

    iF~

    nF~

    iF~

    nF~

    1F~

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    CE 201 - STATICS

    Support for Rigid Bodies Subjected to Two-Dimensional Forces System.

    Table 5 - 1

    Type of Connection Reaction Numbers of Unknowns

    One unknown. The reaction is the tension force which

    acts away from the member in the direction of the cable

    One unknown. The reaction is a force which acts

    along the axis of the link.

    One unknown. The reaction is a force which acts

    perpendicular to the surface at the point of contact.

    One unknown. The reaction is a force which acts

    perpendicular to the slot.

    One unknown. The reaction is a force which acts

    perpendicular to the surface at the point of contact.Rocker

    Roller or pin in confined smooth slot

    Roller

    Weightless Link

    Cable

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    CE 201 - STATICS

    Member fixed

    connected tocollar on smooth rod

    Support for Rigid Bodies Subjected to Two-Dimensional Forces System.

    Table 5 - 1

    Type of Connection Reaction Numbers of Unknowns

    One unknown. The reaction is a force which acts

    perpendicular to the rod.

    Two unknown. The reaction are two components offorce, or the magnitude and its direction of the resultantforce. Note that and are not necessarily equal.(usually not, unless the rod shown is a link as in (2)).

    Two unknowns. The reactions are the couple moment

    and the force which acts perpendicular to the rod.

    Three unknowns. The reaction are the couple and the

    two forces components, or the couple and the magnitude

    and direction of the resultant force.

    One unknown. The reaction is a force which acts

    perpendicular to the surface at the point of contact.

    Fixed support

    Smooth pin or hinge

    Member pin connected to collar on smooth rod

    Smooth contacting surface

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    CE 201 - STATICSDr. Mustafa Y. Al-MandilDepartment of

    Civil Engineering

    LECTURE

    18 336

    FREE BODY DIAGRAM

    EQUILIBRIUM IN 2-DIMENIONS

    FByFBxFB B

    AD

    CFc

    OMo

    Fy

    Fx

    FOR EQUILIBRIUM

    OM

    OF

    OF

    z

    y

    x

    ..(1)

    ..(2)

    ..(3)

    RAx

    RAyFcy RDy

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    CE 201 - STATICSDr. Mustafa Y. Al-MandilDepartment of

    Civil Engineering

    LECTURE

    19 137

    EXAMPLE

    Determine the support reaction in the beam (ABCD).Consider beam weight equals 50N.

    A

    C4

    3

    5100N

    B

    3m 2m 5m

    DX

    A

    B

    C D

    RAx

    RAy

    60N80N

    50N RDy

    SOLUTION

    First we draw FBD for beam (ABCD)

    +

    (1)

    (2)

    Solve (1) & (2)

    RDy = 49N ( ) RAy = 81N( )

    +

    1007R3R-

    07R2503R

    0M

    130RR

    0R5080R

    0F

    )(06R060R

    0F

    DyAy

    DyAy

    B

    DyAy

    DyAy

    y

    N

    Ax

    Ax

    x

    a

    +

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    CE 201 - STATICSDr. Mustafa Y. Al-MandilDepartment of

    Civil Engineering

    LECTURE

    19 238

    A

    B

    C D

    RAx

    RAy

    60N 80N

    50N RDy

    ALTERNATE SOLUTION I

    SOLUTION

    N

    Ay

    Ay

    D

    N

    Dy

    Dy

    A

    NAxAx

    x

    8110

    560250R

    010R780550

    0M

    )(4910

    240250R

    038055010R

    0M

    )(60R060R

    0F +

    +

    +

    CONCLUSION

    0M0

    M

    0F

    D

    A

    x

    One force equationand two moment

    equations on a linenot to the forcedirection.

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    CE 201 - STATICSDr. Mustafa Y. Al-MandilDepartment of

    Civil Engineering

    LECTURE

    19 339

    A B C D

    RAx

    RAy

    100N

    50N RDy

    +4m

    E

    43

    5

    3m 2m 5m

    ALTERNATE SOLUTION II

    CONCLUSION

    0M0

    M

    0M

    E

    D

    A

    Three momentequations taken

    at three points noton a straight line.

    )(60

    4

    240

    4

    250490R

    04R5501049

    0M

    )(81R

    0M

    )(49R

    0M

    N

    Ax

    Ax

    E

    N

    Ay

    D

    N

    Dy

    A

    +

    +

    +

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    CE 201 - STATICS

    Given:

    kA = kB = 15kN/m

    Required:

    c = ?

    40 9.8 = 392N

    A B

    C

    40kg

    392N

    1m 3m

    RA=KAA RB=KBB

    C

    0.1045m

    0.0784m

    m

    C

    C

    m

    A

    AA

    AAB

    y

    m

    B

    BB

    A

    0.6532

    3

    0.1045-

    1

    0.10450.0784

    0.078415000

    1176

    k

    R

    1176R0392RR

    0F

    15680.104515000

    4392

    043921k

    0M

    N

    N

    BR

    +

    +

    A

    B

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    CE 201 - STATICS LECTURE20 2

    41

    TWO FORCE MEMBERS:

    OR

    THREE FORCE MEMBERS:

    AF~

    AF~

    AF~

    AF~

    AF~

    BF~

    BF~

    BF~

    BA

    F~

    F~

    A

    BB

    A

    B

    A

    BF~

    AF~

    BF~

    AF~

    CF~

    CF~

    0F

    0F

    y

    x

    O

    BA

    C

    CF~

    AF~

    BF~

    Dr. Mustafa Y. Al-MandilDepartment of

    Civil Engineering

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    CE 201 - STATICS Dr. Mustafa Y. Al-MandilDepartment ofCivil Engineering

    DISTRIBUTED LOADING

    A) Uniform Distributed Loading:

    B) Linear Distributed Loading:

    C) Trapezoidal Distributed Loading:

    6m 3m

    6m 4m

    5N/m 30N

    45N

    15N/m

    10N/m

    60N

    30N

    20N/m

    6m 4m

    3m

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    CE 201 - STATICS

    Given: Beam ABCRequired: Find Reactions

    )(408040R

    0401005

    4R

    0F

    )(306030R

    0301005

    3R

    0F

    100R

    4004R

    010405R5

    4

    0M

    kN

    Ay

    Ay

    y

    kN

    Ax

    Ax

    x

    kN

    B

    B

    B

    A

    a3

    2d

    2

    ad

    2

    d

    2

    a

    0)2

    d

    2

    a

    (W)2

    a

    (dW

    0Mo

    +

    +

    (

    +

    50kN

    34

    5m

    5m

    3m

    4m

    5mA B

    D

    C

    B CA 5m

    34

    RBRAy

    RAx

    40kN

    30kN

    RB

    RD3m

    4mTwo Force Member

    RB= RD d

    D/2 D/2

    Wa

    o

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    CE 201 - STATICS

    Q.

    Dr. Mustafa Y. Al-MandilDepartment of

    Civil Engineering

    Determine the support reaction of beam ABCD ?3m4m

    B

    D

    CA

    2m

    w = 15N/m3

    4

    50N

    3m4m2m

    RAx

    RByRAy

    A B C60N 40N

    30N

    60Nm

    Free body Diagram

    A. Draw F.B.D.Transfer the (50N) force from point (D) to point (C)

    )(85

    4

    340R

    340602801204R

    06070404R260

    0M

    )(30R

    030R0F

    N

    By

    By

    By

    A

    N

    Ax

    Ax

    x

    )(15

    408560R

    0408560R

    0F

    N

    Ay

    Ay

    y

    +

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    CE 201 - STATICS

    Support for Rigid Bodies Subjected to Three-Dimensional Forces System.

    Table 5 - 2

    Type of Connection Reaction Numbers of Unknowns

    One unknown. The reaction is a force which acts away

    from the member in the direction of the cable.

    One unknown. The reaction is a force which acts

    perpendicular to the surface at the point of contact.

    One unknown. The reaction is a force which acts

    perpendicular to the surface at the point of contact.

    Three unknowns. The reactions are three rectangular

    force components.

    Four unknowns. The reactions are two force and two

    couple components which act perpendicular to the shaft.

    Cable

    smooth surface support

    Roller on a smooth surface

    Ball and socket

    Single journal bearing

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    CE 201 - STATICS

    Support for Rigid Bodies Subjected to Three-Dimensional Forces System.

    Table 5 - 2

    Type of Connection Reaction Numbers of Unknowns

    Five unknowns. The reactions are three force and

    two couple components.

    Five unknowns. The reactions are three force andtwo couple components.

    Five unknowns. The reactions are three force and

    two couple components.

    Six unknowns. The reactions are three force and

    three couple components.

    Single thrust bearing

    Single smooth pin

    Single hinge

    Fixed support

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    CE 201 - STATICSDr. Mustafa Y. Al-MandilDepartment of

    Civil Engineering

    1m

    1.5m

    4m

    D

    A

    C

    B

    y

    x

    z

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    CE 201 - STATICSDr. Mustafa Y. Al-MandilDepartment of

    Civil Engineering

    A

    0.3m

    0.2m

    0.6m

    0.5m

    1m

    0.5m

    100 kg

    C

    B E

    D

    x

    y

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    CE 201 - STATICSDr. Mustafa Y. Al-MandilDepartment of

    Civil Engineeringz

    x

    y

    A

    C

    B

    3ft3ft

    4ft

    6ft

    D

    E

    RAz

    RAx

    8ft

    4ft

    RAyT

    CD

    TCD

    TCE

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    CE 201 - STATICSDr. Mustafa Y. Al-MandilDepartment of

    Civil Engineering

    TRUSSES

    Chep. 6

    Atruss is an assembly of prismaticmembers connected at their ends

    by smooth pin.Forces can only be

    applied at such connections (joints)

    Simple truss:

    Assumptions for Analysis & Design:

    1- Loading and reactions are applied

    at joints (nodes) only. Member weight is

    distributed equally to the adjacent nodes.

    2- Members are loaded at their ends only

    (i.e. two-force members). So, they undergo

    axial forces only (tension or compression). RxyRAy

    RAx

    B

    A C E

    D G

    H

    K

    J

    LECTURE

    23 151

    LECTURE

    23 151

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    CE 201 - STATICS LECTURE 232

    52

    Dr. Mustafa Y. Al-MandilDepartment of

    Civil Engineering

    Analyze the truss shown below:

    )(40R0F

    )(45R0F

    )(45R

    06203204R

    0M

    kN

    Ayy

    kNAxx

    kN

    Bx

    Bx

    A

    F.B.D. For Whole Truss :

    Take Joint (E) :

    (C)15F0255

    3F

    0F

    (T)25F020F54

    0F

    kN

    EDED

    x

    kNECEC

    y

    +

    +

    4m

    RAy

    RAx

    RBx

    A C

    B DE

    3m 3m

    20kN 20kN

    FEC

    FEDE

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    CE 201 - STATICS LECTURE 23

    Analyze the truss shown below:

    252

    Dr. Mustafa Y. Al-MandilDepartment of

    Civil Engineering

    Take Joint (C) :

    (C)20F0F

    (T)15F0F

    kN

    CDy

    kN

    CAx

    Take Joint (A) :

    0

    0505

    440

    0

    )(50

    05

    34515

    0

    AB

    AD

    y

    kN

    AD

    AD

    x

    F

    F

    F

    TF

    F

    F

    +

    FCA

    FCD25kN

    C

    40kN

    45kN 15kNA

    FAD

    FAB

    CE 201 STATICSD M t f Y Al M dil

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    CE 201 - STATICS LECTURE24 1

    53

    Dr. Mustafa Y. Al-MandilDepartment of

    Civil Engineering ZERO-FORCE MEMBERS

    Members which carry no forces in a truss either because of particular

    loading pattern or because they enhance geometric stability:.

    EQUAL-FORCE MEMBERSF3

    F1

    F2

    F2 F1

    F1= F2

    F3

    = 0

    F3

    F1

    F2F4

    F1= F3

    F2= F4

    30kN

    35kN25kN

    30kN40kN

    A

    B

    D I LP

    T

    G K

    C E H J M N Q

    ZERO-FORCE MEMBERS

    BC, BEKM, KN

    PQ, PN, LN

    (C)40F

    (T)25F

    kN

    IJ

    kN

    HG

    CE 201 STATICSD M t f Y Al M dil

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    CE 201 - STATICS

    By sectioning the truss into two or more parts (each part containingmore then one joint), then we can find forces in certain numbers directly.

    LECTURE

    24 254

    Dr. Mustafa Y. Al-MandilDepartment of

    Civil Engineering METHOD OF SECTIONS

    Use Section A-A

    Find FGH ?

    (C)155F

    04F480650

    0M

    kN

    GH

    GH

    J

    80kN

    50kN

    JG

    FGH

    +

    4m

    50kN80kN

    3m

    3m

    3m

    3m

    3

    m

    A A

    F3

    F2

    F1

    0

    0Mo

    F1 =

    CE 201 STATICSD M t f Y Al M dil

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    CE 201 - STATICS LECTURE25 2

    55

    Dr. Mustafa Y. Al-MandilDepartment of

    Civil Engineering THEORY OF PLANE TRUSSES

    M = Number of members

    R = Number of Unknown ReactionsJ = Number of joints

    if M + R > 2J Statically Indeterminate

    if M + R = 2J Statically Determinate

    if M + R < 2J Statically Unstable

    M = 9

    R = 3

    J = 6

    M + R = 2J

    Determinate

    M + R > 2J

    Indeterminate

    M = 10

    R = 3

    J = 6

    M + R < 2J

    UNSTABLE

    M = 8R = 3

    J = 6

    B

    C E

    D

    A G

    CE 201 STATICSDr Mustafa Y Al Mandil

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    CE 201 - STATICS

    Frames are structural systemscomposed of members connected

    and loaded at unrestricted

    locations along their axis.

    LECTURE

    27 158

    Dr. Mustafa Y. Al-MandilDepartment of

    Civil Engineering

    ANALYSIS & DESIGN

    1- SOLVE FOR EXTERNAL REACTIONS

    ( partially or totally ).

    2- DIS-ASSEMBLE & TREAT EACH COMPONENTAS RIGID BODY UNDER EQUILIBRIUM.

    3- FORMULATE SETS OF SIMULTANEOUS

    EQUATIONS & SOLVE FOR UNKNOWNS.

    RAx

    RAy RDy

    A D

    B

    C

    P2

    P1

    M

    RAx RGx

    RAy RGy

    P1

    P3P2

    C

    G

    E

    A

    B

    D

    CE 201 STATICSDr Mustafa Y Al Mandil

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    CE 201 - STATICS

    Analyze Frame (ABCDE)

    LECTURE

    27 258

    Dr. Mustafa Y. Al-MandilDepartment of

    Civil Engineering

    Take whole Frame Take Part (ABC) As F.B.D.

    kN

    Ay

    Ay

    y

    kN

    Ey

    Ey

    A

    25R

    0R4015

    0F

    1512

    180

    R

    03406012R

    0M

    )(3.75

    8

    120150R

    06R8R340

    0M)(15R

    04025R

    0F

    kN

    Ax

    AyAx

    C

    kN

    Cy

    Ey

    y

    Take Whole Frame Again

    )(3.75R03.75R

    0F

    kN

    Exex

    x

    RAy

    A E

    C

    40kN

    60kNm

    REy

    4m

    4m

    DB

    3m3

    m

    3

    m

    3

    m

    RAx

    CRCy

    RAy

    RCx

    A

    B

    45kN

    40kN

    +

    +

    CE 201 STATICSDr Mustafa Y Al-Mandil

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    CE 201 - STATICS LECTURE25 3

    56

    Dr. Mustafa Y. Al-MandilDepartment of

    Civil Engineering GENERAL EXAMPLE

    (a) (b)

    (c) (d)

    (e)

    (g) (h)

    (f)

    Howe Truss Pratt Truss

    Warren Truss Warren Truss with verticals

    K Truss Sub-divided Warren Truss

    Sub-divided Pratt Trussor Baltimore Truss

    Baltimore Truss with inclinedchord or Petit Truss

    (a)

    (d)

    (c)

    (b)

    Howe Truss

    Pratt Truss

    Fan Truss

    Fink Truss

    Conventional Roof Trusses

    Conventional Bridge Trusses

    CE 201 STATICSDr Mustafa Y Al-Mandil

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    CE 201 - STATICS LECTURE25 4

    57

    Dr. Mustafa Y. Al-MandilDepartment of

    Civil Engineering GENERAL EXAMPLE

    CE 201 STATICS LECTUREDr Mustafa Y Al-Mandil

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    CE 201 - STATICS LECTURE28 1

    59a

    Dr. Mustafa Y. Al MandilDepartment of

    Civil EngineeringEXAMPLE

    AnalyzetheFra

    me

    Take whole Frame :

    )(35R

    0R80115

    0F

    )(1158

    920R

    015404808R

    0M

    kN

    Ay

    Ay

    y

    kN

    Hy

    Hy

    A

    +

    )(40R0F

    )(40R

    0M

    kN

    eyy

    kN

    Cy

    E

    Take ( C.D.E. ) :

    +

    RAx RHx

    RAy RHy

    80kN

    C

    H

    G

    A

    B

    E40kN D

    12m

    3m

    6m

    9m

    4m 4m

    RCx C

    RCy

    ED80kN

    REy

    REx

    CE 201 - STATICS LECTUREDr. Mustafa Y. Al-Mandil

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    CE 201 - STATICS LECTURE28 1

    59b

    Dr. Mustafa Y. Al MandilDepartment of

    Civil EngineeringEXAMPLE

    Take whole Frame :

    kN

    Exx

    kNGB

    GB

    y

    kNHx

    Hx

    J

    120R0F

    213.6F

    040F8.54

    3115

    0F

    80R

    015R1640-16115

    0M +

    Analyze the Frame

    RHx

    H

    G

    6m

    9m

    115kN

    FGB

    JREx

    40kN

    16m E

    3

    8

    CE 201 - STATICS LECTUREDr. Mustafa Y. Al-Mandil

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    CE 201 - STATICS LECTURE28 2

    60a

    usta a a dDepartment of

    Civil Engineering

    Analyze the Frame

    Take whole Frame :

    N

    AyAy

    y

    N

    Ax

    Ax

    x

    N

    Ex

    Ex

    A

    100R0100R

    0F

    5461R

    05461R

    0F

    61.54R0810013R

    0M +

    Take Pulley as F.B.D. :

    100N

    100N

    100N

    100N

    100N

    2m6m

    H

    E

    D

    C

    B

    2m

    4m

    5m

    2m

    REx

    RAx

    RAy

    3m

    G

    A

    CE 201 - STATICS LECTUREDr. Mustafa Y. Al-Mandil

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    CE 201 STATICS LECTURE28 2

    60b

    Department ofCivil Engineering

    Take GCH as FBD :

    Analyze the Frame

    G C H 100N

    100NTGB

    RCy

    RCx

    N

    Cy

    Cy

    y

    N

    Cx

    Cx

    x

    N

    GB

    GB

    c

    300R

    0100R2505

    40F

    50R

    0100R2505

    3

    0FT250T

    061003T5

    4

    0M +