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  1. Apply a free-body analysis to the bar BDE to find the forces exerted by links AB and DC. Evaluate the deformation of links AB and DC or the displacements of B and D. Work out the geometry to find the deflection at E given the deflections at B and D. Example 5 (cont’d) SOLUTION: Free body: Bar BDE. ∑ MB = 0.

  2. You use the formula displacement = PL/AE where P=load, L=length of member, A=cross-sectional area tangent to the load, and E=Young's modulus. You get: 500(*1.5m^1/3)^1/3 N/m x 1.5m = 0.00175m^2. Mar 11, 2014

  3. – Make it easy to satisfy dis placement BC using interpolation technique • Beam element – Divide the beam using a set of elements – Elements are connected to other elements at nodes – Concentrated forces and couples can only be applied at nodes – Consider two-node bean element – Positive directions for forces and couples

  4. mathalino.com › reviewer › mechanics-and-strength-of-materialsAxial Deformation | MATHalino

    In the linear portion of the stress-strain diagram, the tress is proportional to strain and is given by $\sigma = E \varepsilon$ since $\sigma = P / A$ and $\varepsilon = \delta / L$, then $\dfrac {P} {A} = E \dfrac {\delta} {L}$ $\delta = \dfrac {PL} {AE} = \dfrac {\sigma L} {E}$ To use this formula, the load must be axial, the bar must have a ...

  5. 20 mar 2011 · This is calculated using the formula d = PL/AE, where d is the end deflection of the bar in meters, P is the applied load in Newtons, L is the length of the bar in meters, A is the cross sectional area of the bar in square meters, and E is the modulus of elasticity in N/m2.

  6. Tensile and compressive stresses are called direct stresses and act normal to the cross-sectional surface. Since stress is directly proportional to force divided by area, and strain (a dimensionless quantity) is related to deflection as. x , ε 1⁄4 L. (1.3) we can now rewrite Hooke’s law as. ε, 1⁄4.

  7. > r := proc (x) r1 + (r2-r1)*(x/L) end; > A := proc (r) Pi*(r(x))^2 end; > Iz := proc (r) Pi*(r(x))^4 /4 end; > Jp := proc (r) Pi*(r(x))^4 /2 end; where r(x) is the radius, A(r) is the section area, Iz is the rectangular moment of inertia, and Jp is the polar moment of inertia.

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