6 of 8H.W.6: For the longitudinal frame of the flat slab floor shown in figure, andby using the Direct Design Method, find:a- Longitudínal distribution of the total static moment at factored loads.b- Lateral distribution of moment at exterior panel (column and middle stripmoments at exterior support). Given w = 18.0kN/m², edge beams:300 x 600 mm.5000 mm6000CL Panel2000CLPanel9400mm-4005000 mmH.W.7: For the transverse exterior frame (Frame D) of the flat plate floor,without edge beams, shown in Figure, and by using the Direct DesignMethod, find:120k H.W.5: For the transverse frame of the flat slab floor shown in figure, and byusing the Direct Design Method, find:a- Longitudinal distribution of the total static moment at factored loads.b- Lateral distribution of moment at exterior panel (column and middle stripmoments at exterior support). Given D = 7.0kN/m², L = 4.0kN /m²500050003005- 1608 009-

Solution Since you have asked multiple questions, we will solve the first question for you. If you…

H.W.6: For the longitudinal frame of the flat slab floor shown in figure, and by using the Direct Design Method, find: a- Longitudínal distribution of the total static moment at factored loads. b- Lateral distribution of moment at exterior panel (column and middle strip moments at exterior support). Given w = 18.0kN/m², edge beams: 300 x 600 mm. 5000 mm 6000 CLPanel boo - 2000 150- CLPanel 8 750- 400 0400mm + 2000 550 250 180 + 000z -ww 0009

H.W.6: For the longitudinal frame of the flat slab floor shown in figure, and by using the Direct Design Method, find: a- Longitudínal distribution of the total static moment at factored loads. b- Lateral distribution of moment at exterior panel (column and middle strip moments at exterior support). Given w = 18.0kN/m², edge beams: 300 x 600 mm. 5000 mm 6000 CLPanel boo - 2000 150- CLPanel 8 750- 400 0400mm + 2000 550 250 180 + 000z -ww 0009

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

The simply supported beam consists of a W460 × 82 structural steel wide-flange shape [E = 200 GPa; I = 370 × 106 mmª]. For the loading shown, determine the beam deflection vc at point C. Assume P = 51 kN, w = 18 kN/m, LAB = LBC = 2.8 m, LcD = 2.2 m. C LẠB LBC LCD mm. Answer: vc =
A beam is subjected to equal bending moments of M₂ = 3200 N-m. The cross-sectional dimensions are b= 145 mm, c = 30 mm, d= 72 mm, and t = 3 mm. Determine: (a) the centroid location (measured with respect to the bottom of the cross-section), the moment of inertia about the z axis, and the controlling section modulus about the z axis. (b) the bending stress at point H. Tensile stress is positive, while compressive stress is negative. (c) the bending stress at point. K. Tensile stress is positive, while compressive stress is negative. (d) the maximum bending stress produced in the cross section. Tensile stress is positive, while compressive stress is negative. M₂ M₂ X (typ) 4 b H K d
The cantilever beam consists of a rectangular structural steel tube shape [E = 29,000 ksi; I = 1570 in.“]. For the loading shown, determine: (a) the beam deflection at point A. (b) the beam deflection at point B. Assume MA = 160 kip-ft, P = 10 kips, LAB = 9.0 ft, LBC = 13.5 ft. MA A В C LAB LBC Answer: (a) VA = in. (b) Ув in.
A beam is subjected to equal bending moments of M, = 3800 N-m. The cross-sectional dimensions are b = 200 mm, c = 30 mm, d = 75 mm, and t = 8 mm. Determine: (a) the centroid location (measured with respect to the bottom of the cross-section), the moment of inertia about the z axis, and the controlling section modulus about the z axis. (b) the bending stress at point H. Tensile stress is positive, while compressive stress is negative. (c) the bending stress at point K. Tensile stress is positive, while compressive stress is negative. (d) the maximum bending stress produced in the cross section. Tensile stress is positive, while compressive stress is negative. M. y M2 H d ((ур) K b
A beam is subjected to equal bending moments of M, = 3900 N-m. The cross-sectional dimensions are b = 190 mm, c= 30 mm, d = 65 mm, and t = 5 mm. Determine: (a) the centroid location (measured with respect to the bottom of the cross-section), the moment of inertia about the z axis, and the controlling section modulus about the z axis. (b) the bending stress at point H. Tensile stress is positive, while compressive stress is negative. (c) the bending stress at point K. Tensile stress is positive, while compressive stress is negative. (d) the maximum bending stress produced in the cross section. Tensile stress is positive, while compressive stress is negative. M2 M2 H d (typ) K Answer: (a) y= 21.67 mm 1055000.021 mm4 %3D mm3 (b) OH= 141.693 MPa (c) OK 61.62 MPа (d) Omax 160.177 MPa e Type here to search
A beam is subjected to equal bending moments of M, = 4300 N-m. The cross-sectional dimensions are b = 140 mm, c = 35 mm, d = 68 mm, and t = 5 mm. Determine: (a) the centroid location (measured with respect to the bottom of the cross-section), the moment of inertia about the z axis, and the controlling section modulus about the z axis. (b) the bending stress at point H. Tensile stress is positive, while compressive stress is negative. (c) the bending stress at point K. Tensile stress is positive, while compressive stress is negative. (d) the maximum bending stress produced in the cross section. Tensile stress is positive, while compressive stress is negative. M2 H d (tур) K Answer: (a) y= i mm Iz = i mm4 S= i mm3 (b) ƠH MPa (c) OK = i MPa (d) Omax i MPa
The simply supported beam consists of a W460 x 82 structural steel wide-flange shape [E = 200 GPa; /= 370 × 106 mm4]. For the loading shown, determine the beam deflection vc at point C. Assume P = 56 kN, w = 22 kN/m, LAB = LBC= 2.9 m, LCD = 2.9 m. P "| พ X C LBC A Answer: Vc= LAB B mm. LCD
The cantilever beam consists of a rectangular structural steel tube shape [E = 29,000 ksi; I-1730 in.4]. For the loading shown, determine: (a) the beam deflection at point A. (b) the beam deflection at point B. Assume MA = 210 kip-ft, P = 13 kips, LAB = 3.8 ft, LBC = 5.7 ft. MA A Answer: (a) VA = (b) VB = LAB P B in. in. LBC C - X
1. A simply supported beam carries three concentrated loads as shown in the figure. a. Determine the slope and deflection equation for every segment of the beam. b. Determine the deflection per El at the right half of the beam. (hint: Eq. - Ely = 54x-2/3x³-5/3[x-67³-6264) c. Determine the value of Ely under the 8-kip load. (Ans: 6246 kip.ft³) 10 kips 8 kips 6 ft 6 ft 6 ft 10 kips 6 ft
34 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.
X Your answer is incorrect. The simply supported beam consists of a W21 x 44 structural steel wide-flange shape [E = 29,000 ksi; I = 843 in.“]. Assume that the support at D can provide resistance %3D either up or down. For a loading of w = 5.4 kips/ft, determine: (a) the beam deflection vg at point A. (b) the beam deflection vc at point C. Assume LAB = 13 ft, LBc = 7 ft, LcD =7 ft, LDE = 6 ft. %3D A B E LAB LBC LcD LCD Lpe Answers: (a) VA = -0.65669 in. (b) vc = 0.024937 in.
USING DOUBLE INTEGRATION METHOD AND MOMENT AREA METHOD DETERMINE THE VALUE OF EI8 AT MIDSPAN FOR THE BEAM LOADED P1 AND P2 ARE IN KN A AND L ARE IN M W ARE IN KN/M L/2 L/2