Structural Analysis
6th Edition
ISBN: 9781337630931
Author: KASSIMALI, Aslam.
Publisher: Cengage,
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- 1)Determine the horizontal and vertical components of the deflection at joint B B A 35 kN 4m 84 kN Plate #5 3m 4m E = 200 Gpa A 1200 mm²arrow_forwardBoth portions of rod ABC are made of aluminum for which E = 70 MPa. Knowing that the magnitude of P = 6 kN and Q = 42 kN determine the diameter d of portion AB for which the deflection of point A will be zero. A - - 0.4 m 0.5 m 60-mm diameterarrow_forwardAt which point on the design P-M interaction diagram is the design flexural strength largest? O Pure compression Pure tension Balanced failure point (CCL limit) O TCL limit Beam condition (Pn = 0) %3D //img00.zhaopin.cmarrow_forward
- A 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_forwardA 30mm diameter bar is 1.25 m long. When the bar is simply supported at its ends in a horizontal position and is loaded with a concentrated load of 370 N at mid span, the central deflection was found to be 9.50 mm. In the second case, the bar is placed vertically and loaded axiallyThe buckling stress (in N/ mm²) of the vertical bar isarrow_forwardDetermine the distribution of the shear stress over the cross section of the beam shown in Fig.aarrow_forward
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