Find the concentrated loads equivalent to the parabolic, triangular and trapezoidal distributed loads acting on the composite beam in the figure. Determine the support reactions at points A, B and the connection forces at hinge G. The function of the parabolic load is q1(x) = 15 x² kN/m, q2 = 300 kN/m, q3 = 100 kN/m, beam spans are a = 3 m and b = 2 m. %3D

Find the concentrated loads equivalent to the parabolic, triangular and trapezoidal distributed loads acting on the composite beam in the figure. Determine the support reactions at points A, B and the connection forces at hinge G. The function of the parabolic load is q1(x) = 15 x² kN/m, q2 = 300 kN/m, q3 = 100 kN/m, beam spans are a = 3 m and b = 2 m. %3D

Structural Analysis

6th Edition

ISBN:9781337630931

Author:KASSIMALI, Aslam.

Publisher:KASSIMALI, Aslam.

Chapter2: Loads On Structures

Section: Chapter Questions

Problem 1P

See similar textbooks

Similar questions

15.what does mean Equivalent Flexural Stiffness of Shear Wall aru
A simply supported wood beam carries a concentrated load of P = 8200 lbs as shown. The beam spans are L1 = 7 ft and L2 = 14 ft. The rectangular cross section has a width of b = 5.5 in. and a depth of d = 14 in. At section a-a, which is xa = 3 ft to the right of pin support A, determine the magnitude of the horizontal shear stress in the wood beam at point K, which is located yk = 4.5 in. below the centroidal z axis. H y Ун a Ук a B K L2 Answer: TK = i psi
Concrete T-beam has been reinforced by bonding a steel plate to its web asshown below. The beam carries a uniformly distributed load of 40kN/m over a simply supported 8m span. Find the maximum deflection of the beam on the assumption that the concrete is fully operative in both tension and compression.(Est = 200kN/mm^2. Econc = 30kN/mm^2; central deflection due uniformly distributed load, total W acting on a simply supported beam of span L= 5WL^3/(384EI)) can someone please answer this question in detail who is confident in this topic with step-by-step calculations & sketch pls. I've asked this question twice now and I've gotten different answers each time so I'm at a bit of a loss. (DONT respond to this if you have already responded previously) Thank you
2. The beam with cross-section shown carries a uniformly distributed load of intensity w over its entire length. Determine w if the allowable stresses are g = 40 MPa, g = 80 MPa, and t = | T 12 MPa. w (kN/m) 75 mm 10 mm 0.5 m : 10 mm 3m 10 mm- 150 mm 150 mm
Need help ASAP Determine the max flexural stress in MPa
only typed solution accepted
Considering the fully restrained beam shown in Figure 2 where E = 200 GPa and I = 2x10^9 mm^4 If P = 70 kN, M = 100 kNm, L = 12 m., and G = 40 degrees. Use either the virtual work method or the method of consistent deformation and state what you use with a complete solution. thank you. 1. Determine the maximum positive and negative shear that is acting on the beam. 2. Determine the maximum positive and negative moment that is acting on the beam 3. Determine the maximum deflection of the beam. 4. If the maximum deflection is limited to 10mm, determine the diameter of the circular beam required.
Calculate the force generated in element 1 of the following reinforcement if P = 981 N and H = 1.1 m
A T-shape beam is subjected to a vertical shear force of V = 30 kN. The beams centroid is located 211.1 mm above the bottom surface of the beam, and the moment of inertia is l₂ = 48.7 x 106mm4.[b = 178 mm, h = 300 mm, t₁ = 12.7, tw = 9] b h tw Determine the shear stress in the flange at the intersection of the flange and the web. 6.96 MPa 7.6 MPa 2.94 MPa 4.3 MPa 6.09 MPa
Please fast answer
A 3-m span cantilever beam carries a uniformly distributed load of 36 KN/m over its entire length. The beam has a rectangular cross-section with height h twice its width b. The allowable stresses are: flexure stress, fb ≤ 30 MPa and shearing stress, fv ≤ 3 MPa. Determine: The maximum shear force along the length of the beam (in KN).
A Universal beam of I shaped cross-section is 203 mm deep, and 133 mm wide and has a steel plate 150 mm by 10 mm thick fastened to each flange. Ix-x for the universal beam is 28.80×10^6 mm^4. a) Determine the total uniformity distributed load which may be carried over a simply supported span of 6 metres if the permissible bending stress is 165 N/mm^2. Neglect the self-weight of the beam. [Ans.: 124.02 KN/m] b) Determine the minimum central length over which the additional plates are required. [Ans.: 4.23m]