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1.Equilibrium of Deformable Body

Jun 03, 2018

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    Mechanics of Solids (VDB1063)

    Equilibrium of Deformable Body

    Lecturer: Dr. Montasir O. Ahmed

    Universiti Teknologi PETRONASCivil Engineering Department

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    LECTURE OUTLINES

    Introduction

    Equilibrium of Deformed Body

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    Mechanics of materialsis a branch of mechanics that studies the internal effects of stress

    and strainin a solid body that is subjected to an external loading.

    Stressis associated with the strength of the material from which the body is made, while

    strainis a measure of the deformation of the body.

    INTRODUCTION

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    Surface Forces: Caused by the direct contactof one body with

    the surface of other. The resultant force FR acts through the

    centroid Cor geometric centre of this area.

    A body force: is developed when one body exerts a

    force on another body without direct physical contact

    between the bodies such as the earths gravitation

    whereas the force is called weightand acts through the

    bodyscentre of the gravity.

    Equilibrium of Deformable Body

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    Support reactionsare forces that develop at the supports or point of contact between bodies.

    If the supportprevents translationin a given direction, then aforce must be developedon the

    member in that direction. Likewise, if rotation is prevented, a couple moment must be

    exerted on the member.

    Equilibrium of Deformable Body

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    Equation of Equilibrium

    In general, equilibrium of body requires:

    1. Balance of forces to prevent the body from translating. = 0

    2. Balance of moments to prevent the body from rotating. = 0

    If anx,y,zcoordinate system is established with the origin at point O, then the equation

    of equilibrium become:

    = 0, = 0, = 0, = 0 , = 0, = 0

    If the forces lie in the x-y plane (coplanar forces), then the conditions for equilibrium of

    the body can be specified as:

    = 0, = 0, = 0

    The best way to account for all these forces is to draw the bodysfree-body diagram.

    Equilibrium of Deformable Body

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    Internal Resultant Loadings

    The criteria for determination of the internal loadingsis:

    1. Pass an imaginary sectionthrough the region where the internal loadings

    are to be determined (Fig. a).

    2. Draw thefree body diagram of one of the parts as shown in Fig. b.

    3. Use the equations of equilibrium to relate the external forces in the free

    body diagram to the distributionsresultant internal forces and moments,

    and

    Equilibrium of Deformable Body

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    Four different types of internal resultant loadings can

    then be defined as follows:

    1. Normal Force, N: This force acts perpendicular to the

    area. It is developed whenever the external loads tend to

    push or pull on the two segments of the body.

    2. Shear Force, V: This force lies in the plane of the area

    and it is developed when the external loads tend to

    cause the two segments of the body to slide over one an

    other.

    3. Torsional Moment or Torque, T: This effect is developedwhen the external loads tend to twist one segment of the

    body with respect to the other about an axis

    perpendicular to the area.

    4. Bending Moment, M: It cause by the external loads that

    tend to bend the body about an axis lying within the

    plane of the area

    Equilibrium of Deformable Body

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    Important Points in the Lecture

    External forces can be applied as distributed, concentratedsurface loading and body

    forces.

    Linear distributed loadings produce resultant force having magnitudeequal to the area

    under the load and having a locationthat passes through the centroidof this area.

    A support produces aforceif itprevents translation, and it produces a couple moment

    on the member if itprevents rotation.

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    = 0 and = 0 must be satisfied in order topreventa body from translatingand

    from rotating.

    When applying the equations of equilibrium, itsimportant to first draw thefree body

    diagram.

    Method of sections is used to determine the resultant normal force, shear force,

    torsional moment, and bending moment.

    Important Points in this Lecture

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    Stress

    Normal Stress

    Shear Stress

    Design of Simple Connections

    allowable stresses

    Strain

    Normal strain

    Shear strain

    Next Class

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    Thank You