
Structural Analysis
6th Edition
ISBN: 9781337630931
Author: KASSIMALI, Aslam.
Publisher: Cengage,
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Transcribed Image Text:A beam of uniform cross-section, simply
supported at ends carries a concentrated load
W at mid-span. If the ends of the beam are fixed
and only load P is applied at the mid-span such
that the deflection at the centre remains the
same, the value of the load P will be
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- Obtain an expression for the deflection curve of the simply supported beam of Fig. 8-7 subject to the uniformly distributed load w. W mmmmm Fig. 8-7 Determine the maximum deflection of above beam if E=100GPa ● W=200N/m L=4m Rectangular beam section 2cmx8cm (W x D) In addition, you are asked to, W ● Evaluate the types of connection that will be needed to provide the simply supported design ● Discuss the relationship between bending shear, and deflection. • Evaluate steel and reinforced concrete and their structural efficiency in managing bending shear, and deflection. Answer All Questions.arrow_forward04. The load Q is gradually increased from zero to 120kN. a) Does failure occur in bars BE and BD? b) Determine the maximum deflection at pointB. a = 0.64m Square Cross-Section 10mm x 10mm 1.7m E A36-Carbon Steel A36-Carbon Steel 2.64 m OD for all pins = 6mmarrow_forwardA simply supported beam is 0.6 feet long, and has a distributed load of 8.9 kips/ft pointing in the negative y direction along the entire beam. First- find the maximum moment in the beam? HINT: You should draw the beam. QUESTION: If the y distance from the neutral axis to the furthest fiber in tension is = -5 inches, and the moment of inertia of the beam is 100 in4, then what is the bending stress in the beam? in psi? Give answer to 1 decimal point, and no units, such as 1250.1 (not 1250.1 psi)arrow_forward
- Find the flexural stiffness of a simply supported beam, which has a uniform distributed load is (400 N/m), and limits the deflection to (1 mm) at middle. The length of beam (2 m).arrow_forwardA cantilever beam with the fixed support on the left is under the loadings below, w = 3wo. Note: wo, E (Young's modulus), I (moment of inertia) are constant. Click here to see all formulas a a Part A - una? EI Determine the slope of the beam at x = a is assuming w = 3wn. O -0.619 O -1.65 O -1.03 O -1.29 O -0.413 Submit Request Answer una4 X EI Part B - Determine the deflection of the beam at r = a is assuming w = 3wo O -4.62×10-2 O -0.132 O -6.60×10-2arrow_forward34 3 Example 1: i moment My, the plastic c or nominal petermine the yield moment Mp (Mn), and the plastic modulus Z for the simply supported beam having the cross section shown in the figure. Also calculate the shape factor, and nominal load Practing transversely through the mid span of the beam. Assume that F, = 50 ksi. 12 ft Pr -- 12 ft 1 in 15 in. 8 in. 15 in. 17 in. in.arrow_forward
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