The state of stress at a point in a member is shown on the element. Determine the absolute normal stres component acting on the inclined plane AB in ksi. 4 ksi А 3 ksi 19 2 ksi B
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- A beam is supported by hinge at A and roller at B with a span of 10meters section C is 3.75m from support A, the beam is traversed by a uniformly distributed load of 20KN/m extending over a length of 4m. Determine the maximum moment at section C.The beam carrying the 1200lb.ft couple at its midpoint is built in at both ends. Find all the support reactions using double integration method.A beam is supported by hinge at A and roller at B with a span of 10meters section C is 3.75m from support A, the beam is traversed by a uniformly distributed load of 20KN/m extending over a length of 4m. Determine the maximum shear force at section C.
- A simply supported beam AB = 10 m has a hollow rectangular cross-section with 10 cm as width, 23 cm as depth and inner thickness as 2 cm is subjected to a point load of 8 N & 9 N acting at C and D respectively and a uniformly distributed load (UDL) of 8 N/m starts from mid-span and ends at the right support of the beam. Determine the maximum bending stress and the bending stress at 2 cm from the top. Take AC = 1 m & CD = 1 m. iv) Maximum Bending Moment (Please write the Maximum bending moment valve in "Nm") = v) Moment of Inertia, I = vi) Maximum bending stress = vii) Bending stress at 2 cm from the top =A beam ABCDE is 10 m long and is simply supported at B and the extreme right-hand endE. The beam carries point loads of 50 kN on the over-hanging end at A and 60 kN at D,together with a uniformly distributed load of 40 kN/m between B and C. AB = DE =2m, and BC = 4m. If the point C is 2 mm below the level of the supports at B and E.Determine:(a) The flexural stiffness EI. (b) The deflection at the end A.A simply supported beam of length L is load with a moving concentrated load P passing across the span of the beam. Determine the maximum shear force that will carried by the beam. a) P b) P/2 c) P/4 d) 0
- A simply supported beam AB = 10 m has a hollow rectangular cross-section with 17 cm as width, 28 cm as depth and inner thickness as 2 cm is subjected to a point load of 7 N & 5 N acting at C and D respectively and a uniformly distributed load (UDL) of 8 N/m starts from mid-span and ends at the right support of the beam. Determine the maximum bending stress and the bending stress at 2 cm from the top. Take AC = 2 m & CD = 2 m. i) Reaction force at B in (N)= ii) Reaction Force at A in (N) = iii) The distance from B at which the shear Force value changes from "-" to "+" in (m) = iv) Maximum Bending Moment (Please write the Maximum bending moment valve in (Nm) = v) Moment of Inertia, I in (m^4)= vi) Maximum bending stress in (N/m^2)= vii) Bending stress at 2 cm from the top in (N/m^2) =determine the positive and negative moments of the beam shown. Also, determine the design shear forces at a distance 0.53m from support B in the interior span. The dead and live loads are 24.3 kN/m and 11.2 kN/m.II. If the beam carries a moving uniform load of FN kN/m and concentrated moving load of 118 kN Using theinfluence line diagram, (a) determine the max. +M due to loads at C (b) det. max +V at C
- 3. A 7-meter simple beam has one of its supports at the left end and the other is placed 3m from the right end carrying a triangular load of 0 to 18kN/m that varies 0 kN/m at the left support and terminates with 18 kN/m at the second support. Exactly at the free end, the beam is also carrying a concentrated load of 20 kN. What is the maximum negative moment in the beam?A truss is loaded with nodal force at C as shown TOS-003. If the truss members have identical rectangular section of 5 cm x 8 cm, with E = 70 GPa, compute the vertical displacement at joint C .A propped cantilever beam has a span of 6.0 m. The beam carries a uniform load of 600 kN/m. along the 2.0 m length of the span from the fixed end. Compute the moment at the fixed end in kN.m. a. 833.33 b. 222.33 c. 564.88 d. 933.8