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Structural Analysis: Space Truss - IIT Guwahati

Structural Analysis: Space TrussSpace Truss -6 bars joined at their ends to form the edges ofa tetrahedron as the basic non-collapsible unit-3 additional concurrent bars whose ends are attached to three joints on the existing structureare required to add a new rigid unit to extend the center lines of joined members intersect at a point Two force members assumption is justified Each member under Compression or TensionA Space Truss formed in this way is called a Simple Space Truss1ME101 -Division IIIK austubh DasguptaSpace Truss Analysis: Method of Joints Method of Joints All the member forces are required Scalar equation (force) at each joint Fx= 0, Fy= 0, Fz= 0 Solution of simultaneous equations2ME101 -Division IIIK austubh DasguptaSpace Truss Analysis: Method of Sections Method of Sections A few member forces are required Vector equations (forceand moment) F =0, M =0 Scalar equations 6 nos.

Space Truss Analysis: Method of Joints • Method of Joints –All the member forces are required –Scalar equation (force) at each joint • F x = 0, F y = 0, F z = 0 –Solution of simultaneous equations ME101 - Division III Kaustubh Dasgupta 2

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Transcription of Structural Analysis: Space Truss - IIT Guwahati

1 Structural Analysis: Space TrussSpace Truss -6 bars joined at their ends to form the edges ofa tetrahedron as the basic non-collapsible unit-3 additional concurrent bars whose ends are attached to three joints on the existing structureare required to add a new rigid unit to extend the center lines of joined members intersect at a point Two force members assumption is justified Each member under Compression or TensionA Space Truss formed in this way is called a Simple Space Truss1ME101 -Division IIIK austubh DasguptaSpace Truss Analysis: Method of Joints Method of Joints All the member forces are required Scalar equation (force) at each joint Fx= 0, Fy= 0, Fz= 0 Solution of simultaneous equations2ME101 -Division IIIK austubh DasguptaSpace Truss Analysis: Method of Sections Method of Sections A few member forces are required Vector equations (forceand moment) F =0, M =0 Scalar equations 6 nos.

2 :: Fx, Fy, Fzand Mx, My, Mz Sectionshould notpass through more than 6 members More number of unknown forcesSpace Truss : ExampleDetermine the forces acting in members of the Space :Start at joint A: Draw free body diagramExpress each force in vector notation4ME101 -Division IIIK austubh DasguptaSpace Truss : ExampleRearranging the terms and equating the coefficients of i, j, and kunit vector to zero will give:Next Joint B may be -Division IIIK austubh DasguptaSpace Truss : ExampleUsing Scalar equations of equilibrium at joints D and C will give:Joint B: Draw the Free Body DiagramScalar equations of equilibrium may be used at joint B6ME101 -Division IIIK austubh DasguptaRecapitulation:: Support Reaction7ME101 -Division IIIK austubh DasguptaRecapitulation:: Support Reaction8ME101 -Division IIIK austubh DasguptaRecapitulation:: Free Body Diagram9ME101 -Division IIIK austubh DasguptaRecapitulation:: Free Body Diagram10ME101 -Division IIIK austubh DasguptaRecapitulation:: Method of SectionsMethod of Sections Find out the reactions from equilibrium of whole Truss To find force in member BE: Cut an imaginary section (dotted line) Each side of the Truss section should remain in equilibrium11ME101 -Division IIIK austubh Dasgupta Calculate the force in member DJExample: Method of Sections12ME101 -Division IIIK austubh DasguptaDirection of JK :: Moment @ CDirection of CJ :: Moment @ AExample.

3 Method of Sections13ME101 -Division IIIK austubh DasguptaFrames and MachinesA structure is called a Frame or Machine if at least one of its individual members is a multi-force member member with 3 or more forces acting on it, or member with 2 or more forces and 1 or more couple actingFrames: generally stationary and are used to support loadsMachines: contain moving parts and are designed to transmit and alter the effect of forces actingMulti-force members:the forces in these members in general will not be along the directions of the members methods used in simple Truss analysis cannot be used14ME101 -Division IIIK austubh DasguptaFrames and MachinesInterconnected Rigid Bodies with Multi-force Members Rigid Non-collapsible structure constitutes a rigid unit by itself when removed from its supports first find all forces external to the structure treated as a single rigid body then dismember the structure & consider equilibrium of each part Non-rigid Collapsible structure is not a rigid unit by itself but depends on its external supports for rigidity calculation of external support reactionscannot be completed until the structure isdismembered and individual parts are

4 -Division IIIK austubh DasguptaFrames and MachinesFree Body Diagrams: Forces of Interactions force components must be consistently represented in opposite directions on the separate FBDs (Ex: Pin at A). apply action-and-reaction principle (Ex: Ball & Socket at A). Vector notation: use plus sign for an action and a minus sign for the corresponding reactionPin Connection at ABall & Socket at A16ME101 -Division IIIK austubh DasguptaFrames and MachinesExample: Free Body DiagramsDraw FBD of(a)Each member(b)Pin at B, and (c)Whole system17ME101 -Division IIIK austubh DasguptaExample on Frames and MachinesCompute the horizontal and vertical components of all forces acting on each of the members (neglect self weight)18ME101 -Division IIIK austubh DasguptaFrames and MachinesExample Solution.

5 3 supporting members form a rigid non-collapsible assemblyFrame Statically Determinate ExternallyDraw FBD of the entire frame3 Equilibrium equations are availablePay attention to sense of Reactions19ME101 -Division IIIK austubh DasguptaFrames and MachinesExample Solution: Dismember the frameand draw separate FBDs of each member-show loads and reactions on each memberdue to connecting members (interaction forces)Begin with FBD of PulleyAx= kN Ay= kN D= kNThen draw FBD of Members BF, CE, and AD20ME101 -Division IIIK austubh DasguptaFrames and MachinesExample Solution:FBDsAx= kN Ay= kN D= kNCE is a two-force memberDirection of the line joining the two points of force application determines the directionof the forces acting on a two-force of the member is not -Division IIIK austubh DasguptaFrames and MachinesExample Solution:Find unknown forces from equilibriumMember BFMember CE[ Fx = 0]Cx= Ex= kNChecks:22ME101 -Division IIIK austubh Dasgupta


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