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AERSP 301 Shear of closed section beams Jose Palacios
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Shear of closed section beams Consider the closed section beams subjected to shear loads S x and S y that cause bending stresses and shear flows Equilibrium relation: y x z SxSx SySy S
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Shear of closed section beams As with the open-section beam: Unlike the open-section case – you start at an open end, s = 0, q = 0 – it is generally not possible to choose an origin for s at which the shear flow is known. Assume that for the origin chosen (s = 0), shear flow has value q s,o (unknown).
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Shear of closed section beams First two terms on the RHS represent shear flow in an open section beam loaded through its shear center. Call that q b (“basic” shear flow) q b is obtained by introducing a cut at some convenient point in the closed section, thereby converting it to an open section The value of shear flow at the cut (s = 0) is found by equating applied and internal moments about some convenient moment center.
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Shear of closed section beams The value of shear flow at the cut (s = 0) is found by equating applied and internal moments about some convenient moment center. From the figure A – enclosed area
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Shear of closed section beams If moment center is chosen to coincide with the lines of action of S x and S y then: Above equation can be used to obtain q s,o This expression can be used to find the shear center: Needed in problem 2 Hw 3
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Twist and warping of shear loaded closed section beams Shear loads not applied through the shear center of a closed section beam causes it to twist and warp (warping = out of plane axial displacements) Expressions for twist and warping can be derived in terms of shear flow:
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RECALL! Center of Twist Equivalent to pure rotation about some pt. R (center of twist [for loading such as pure torsion]) For the point N Origin O of axes chosen arbitrarily, and axes undergo disp. u, v,
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Twist and warping of shear loaded closed section beams (cont’d) Previously Integrate w.r.t. s from the origin for s dxdy 2A 0s
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Twist and warping of shear loaded closed section beams cont… A os area, swept by generator, center at origin of axes, O, from origin for s to any point s. Integrating over the entire c/s yields:
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Twist and warping of shear loaded closed section beams Substituting for and rearranging terms: If the origin coincides with center of twist, R, then last two terms on RHS are zero.
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Twist and warping of shear loaded closed section beams (cont’d) In problems with singly or doubly symmetric sections, the origin for s may be taken to coincide with a point of zero warping –This occurs at points where axis of symmetry crosses a wall of the section It is assumed that the direct stress distribution attributed to the axial constraint is proportional to the free warping of the section – = constant x w Since a pure torque is applied, resultant of any internal direct stress must be zero. Thus
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Shear center of closed section beams As with the open section beam, apply a shear load S y and find the coordinate s of the shear center. First you have to determine the shear flow, q s To determine q s,o use the condition that the shear load through the shear center produces zero twist
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Shear center of closed section beams This gives: If Gt = const, then: This expression can also be used to find the shear center
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Sample Problem For the closed section beam shown, calculate the shear center. Y-location of shear center? Symmetry? I xy = ? What load should be applied, S x or S y ?
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Sample Problem Need to Find I xx : 8a 6a 10a S1S1 y
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8a 6a 17a S2S2
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Sample Problem Shear Flow q 1 for S 1 = 10a y Evaluate A and B at beginning and end of path Do you want me to demonstrate this?
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Sample Problem Integrating The shear flow, q, on walls 23 and 34 follow from symmetry. So far we have obtained the basic shear flow (like we did for open cross-section) Now we need to find q s,0
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Sample Problem To obtain q s,0 we use: For the given cross-section Evaluating the Integral: 1 4 2 q 12 q 41 9a ξsξs q 12 q 41 The Shear Flow Becomes:
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Sample Problem To find the shear center let the clockwise moments (due to q 41 ) be equal to the Counter clockwise moments (due to q 12 ) and solving for ξ s : Sum of the moments around what point? 1 4 q 12 q 41 9a ξsξs 2 53 0 28 0
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Sample Problem 0.799 0.4695 Shear Center INSIDE the beam cross-section
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