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- In the beam, which is given the loading and supporting status below a) Find the location of the largest crash and the value of the crash. b) What is the maximum length of the beam (L) so that the largest collapse value is less than 1.5 mm? E = 210 GPa Mo = 250 kNm I = 556x10-6 m4Two elastic beams with equal bending rigidity of EI are connected by a pin at B. The beam is fixed at A and a roller support is attached at C. Beam BC is subjected to a uniformly distributed load of magnitude w=1 N/m. If the bending rigidity EI is 108Nmm2, determine a) the lateral deflection at B, b) the rotational angle at B, c) the rotational angle at C. d) sketch the deformed shapeFor the simply supported beam carrying the concentrated load P = 276 N at its midspan, determine the magnitude of the maximum slope angle of the beam (in degrees) if d = 2.16 m, E = 12.77 GPa , and I =1681393mm4. NOTE: PLEASE ANSWER IT CORRECTLY. IF YOU ARE NOT SURE ABOUT THE ANSWER, PLEASE SKIP THE QUESTIONPLEASE BOX THE FINAL ANSWER(S)THANK YOU!
- The beam safely supports shear forces and bending moments of 2kN and 6.5 kN-m respectively. Based on this criterion, can it be safely subjected to the loads F = 1kN and C = 1.6 kN-m? Use the area methodPlease help me for the correct solution. A leaf spring carries a central load of 3000 N. The leaf spring has to be made of 10 steel plates 5cm wide and 6mm thick. If the bending stress is limited to 150 N/mm² determine: (i) Length of the spring and (ii) Deflection at the centre of the spring. Take E = 2 * 10 ^ 5 * N / m * m ^ 2..?Question 1) F=11 kN single load, M=22 kN.m moment andA distributed load of w=5 kN/m is effective. The length L is also given as L=5 m.The cross-sectional properties of the beam are; body height Hg=218 mm, body thickness xg=18 mm, flangewidth xf=190 mm, flange height yF13 mm. Point E on the section is flange-It is located just below the body junction. In the section taken from the B line of the beamIt is desired to determine the stress state. According to this;Question 1-A) Find the support response (DY) at point D. (Return your result in kNQuestion 1-B) Find the support response (Ay) at point A. (Return your result in kNwrite.)Question 1-C) Find the shear force (VB) at point B. (KN your resulttype in size.)
- The load on a cantilever beam AB has a triangulardistribution with maximum intensity q0 (seefigure). Determine the angle of rotation θB and thedeflection δB at the free end.For the simply supported beam carrying the concentrated load P = 268 N at its midspan, determine the magnitude of the maximum displacement (in mm) if d = 1.51 m, E = 11.77 GPa , and I =1679930mm4. NOTE: PLEASE ANSWER IT CORRECTLY. IF YOU ARE NOT SURE ABOUT THE ANSWER, PLEASE SKIP THE QUESTIONPLEASE BOX THE FINAL ANSWER(S)THANK YOU! image below for referenceFor the beam and loadingshown below, derive an expressionfor the reaction force at B. Assumethat EI is constant for the beam.(Reminder: The roller symbolimplies that both upward anddownward displacement isrestrained.)FIGURE P11.28
- Determine the maximum deflection of the simply supported beam. E = 200 GPa and I = 39.9(10-6) m4.The beam is made of elastic perfectly plastic material for which sY = 345 MPa. Determine the maximum elastic moment and the plastic moment that can be applied to the cross section.Determine the equivalent stiffness of a cantilever beam which is loaded transversely on its end and has a length in 5000 mm and an annular cross section with inner and outer diameters of 25 mm and 22 mm, respectively. The modulus of elasticity of the beam is 72x109 N/m2. Use moment of inertia I=π(D4o−D4i)/64 and spring constant is (k= 500 N/m). Answer must be in three decimal places.