- Concrete weight: wt = 150 pcf - Concrete compressive strength: f'c = 4000 psi - Steel tensile strength: fy = 60 ksi - Stirrup consists of #4 bar - Framing members are not exposed to weather or in contact with soil. Determine the magnitude of the factored point load assuming the dead load = 150psf and live load = 60psf Note: Load factor: U = 1.2D + 1.6L 30-0¹ a= X 83 Column- 899 30-0 Dean- -Sab Mark B4 D4 3 B3 PD & PL L= B 30-0¹ BI D2 BI -Girder PD & PL a= Tre re 13-4 05 40-0¹

- Concrete weight: wt = 150 pcf - Concrete compressive strength: f'c = 4000 psi - Steel tensile strength: fy = 60 ksi - Stirrup consists of #4 bar - Framing members are not exposed to weather or in contact with soil. Determine the magnitude of the factored point load assuming the dead load = 150psf and live load = 60psf Note: Load factor: U = 1.2D + 1.6L 30-0¹ a= X 83 Column- 899 30-0 Dean- -Sab Mark B4 D4 3 B3 PD & PL L= B 30-0¹ BI D2 BI -Girder PD & PL a= Tre re 13-4 05 40-0¹

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

Current Attempt in Progress The cantilever beam consists of a rectangular structural steel tube shape [E = 29,000 ksi; = 1990 in."). For the loading shown, determine: (a) the beam deflection at point A. (b) the beam deflection at point B. Assume MA= 250 kip-ft, P= 14 kips, LAB = 4.1 ft, LBc = 6.2 ft. MA LAB LBC Answer: in. (a) VA- in. (b) VB - 4. Submi Attempts: 0 of 1 used Save for Later
As shown in the figure, a 3m-long cantilever beum is subjected to a uniformly distributed dead load, we-1.S t/m. It is know that f = 20MP. fy =420 MPa, and 4, = 1800 mm. Please find the maximum allowable uniformly distributed live load, wt is assumed that the unit weight of concrete is we24 t/m. -300m-
A lightly welded steel beam shown in Figure 5 is continuously supported along its length. A downward concentrated load of 4P acts at Point C, and two downward concentrated loads P act at Points A and E. The beam with full lateral restraint is bent about its major principal x-axis. Determine the followings: a. Section type based on section slenderness; b. Effective section modulus; c. The maximum design value of P. A k B fu 6 m d tw bf 6 m tf 4P d bf tw tf = - = fyf= fyw 6 m D um * 550 mm 206 mm 6 mm 10 mm 320 MPa = 340 MPa Zx=1362985 mm³ Sx 1533750 mm³ Figure 5 Steel beam under design loads. 6 m P E
The standard load is 100kN. Given that n=4 and α=1, calculate EALF 80.
The simply supported beam consists of a W460 x 82 structural steel wide-flange shape [E = 200 GPa; I = 370 x 106 mm*). For the loading shown, determine the beam deflection vc at point C. Assume P = 56 kN, w = 22 kN/m, Lag = Lsc= 2.9 m, Lco = 2.9 m. LAB LBC LCD Answer: Vc= mm.
Question 3 of 10 View Policies Current Attempt in Progress Answer: Wo A The steel beam has the cross section shown. The beam length is L = 5.8 m, and the cross-sectional dimensions are d = 400 mm, bf = 210 mm, tf = 14 mm, and tw = 7 mm. Calculate the largest intensity of distributed load wo that can be supported by this beam if the allowable bending stress is 160 MPa. A 72 Save for Later Wo B 72 C kN/m - / 10 E ||| d 600 Attempts: 0 of 3 used Submit Answer
The steel beam has the cross section shown. The beam length is L = 7.3 m, and the cross-sectional dimensions are d = 300 mm, bf = 180 mm, tf = 13 mm, and tw = 7 mm. Calculate the largest intensity of distributed load w0 that can be supported by this beam if the allowable bending stress is 250 MPa.
simply supported beam AB has a length of 3 m and carries distributed load which varies in linear manner from (1w) N/m at A support to (2w) N/m at the B support and concentrated load (1.5w) N at 2 m from A support, and the beam has hollow circular cross section of diameter ratio diu/dow =1/3. Draw S.F. and B.M. diagrams for the beam and determine the value of (w) if the maximum bending stress 110 Nam?, and the average shear stress at 1 m from point A equal to 15 N/m. COMPANY
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
Current Attempt in Progress For the beam shown, calculate the beam slope at D. Assume that a = 4.4 ft, b = 6.6 ft, c= 8.8 ft, w = 1700 lb/ft, P = 2500 lb, and El = 528000 kip-in.². A Answer: OD i a Save for Later W B b P ITIV rad с C D
Determine the load capacity of the angle LRFD. USE NSCP 2015.
! Required information Consider the beam and loading shown. Given: X = 25 kips X 을 in. |n 7.25 in. A B $1.5 in. 1,5 in. 20 in. -을 in. 20 in.- in.- 10 in. 8 in.- Determine the shearing stress at point a. (Round the final answer to three decimal places.) The shearing stress at point a is |ksi