Determine the maximum flexural stresses in the Tee Beam (Fig. 5) and the locations where it occurs. The beam is loaded as shown below. Draw moment diagram first. Value of P is given beside the figure for differing Rolls numbers. Rolls Even P 200 mm 7.P kN or Odd P kN/m 50 mm Even Rolls 2.5 200 A Odd Rolls 3 50 Beam Sec. 4 m 4 m 6 m

Determine the maximum flexural stresses in the Tee Beam (Fig. 5) and the locations where it occurs. The beam is loaded as shown below. Draw moment diagram first. Value of P is given beside the figure for differing Rolls numbers. Rolls Even P 200 mm 7.P kN or Odd P kN/m 50 mm Even Rolls 2.5 200 A Odd Rolls 3 50 Beam Sec. 4 m 4 m 6 m

Steel Design (Activate Learning with these NEW titles from Engineering!)

6th Edition

ISBN:9781337094740

Author:Segui, William T.

Publisher:Segui, William T.

Chapter3: Tension Members

Section: Chapter Questions

Problem 3.3.1P

See similar textbooks

Similar questions

None
please include the FBD
Compute the compressive strength of a WT 12x81 of A992 steel. The effective length with respect to the x-axis is 25 feet 7inches, the effective length with respect to the y axis is 20feet, and the effective length with respect to the z-axis is 20 feet WT12X81 A 23.9 t₁ 1.22 ly 221 d 12.5 K des 1.72 J 9.22 b₁ 13.0 y 2.70 Cw 43.8 tw 0.705 Ix 293
For the beam and loading shown, calculate (a) the equation of the elastic curve, (b) the deflection at point B, (c) the deflection at point C. A | 12 B L./2 Wo IC X
Notes: Answer five questions including sixth question Q1/ Two Forces Shown in Fig. (1) acts on the bracket, determine the effect of these two forces (using Parallelogram method). Maloyan an syurvalet sy siera consists (Single Force & Couple al pont. Ajo 100 F₂ = 150N -10MCHIL DENG F₁ = 200 N Fig. (1) is 4XKSA
Required information Consider the loading condition shown. Assume that the flexural rigidity El of the beam is constant. 21 W B -L/2L/2L/2- The deflection at point B is. 0013 W Using singularity functions, determine the deflection at point B and point D. (Round the final answers to four decimal places.) The deflection at point Dis. -0.0163 wwwwwwwwww………… 1 D x Deflection point at D is wrong
Show detailed solution refer to the table of equations.
Determine the type and amount of stress in each member of the truss shown below due to wind load using the method of joints. a.) Draw FBD b.) Solve the stress of all the members c.) Tabulate your answers (Length, Force, Compression/Tension, etc.)
Find the member forces required. Indicate if members are in compression. Required:member forces AH AC CD CH DE BE CG BF DG. ANSWERS UP TO 5 DECIMAL PLACES
For the beam below, determine the following, assume EI is constant. What is FEMAB in k-ft? -18 --96 Select the correct response: -69 2 k/ft 18 24ft
Check the adequacy of column AB for applied live load. Fy= 350Mpa W360x51: A= 6450mm2 rx= 148mm ry= 38.8mm d=355mm b=171mm == 11.6mm =7.2mm 2m B F W360x51 A 3m GookN/m (Live load) D c 3m Md Sof EX
Using the area method, DRAW THE SHEAR AND BENDING MOMENTS DIAGRAM 206 N/m 310 N/m matent or co unic ac "The tect proper dy the wichin 250 N 2m 2m 5m Use the template below for your solutions: Shear Calculation Relation of Shear to Concentrated and Distributed Load VB-VA = Bending Moment Calculation Relation of Bending Moment to Applied Moment and Shear Diagram MB - MA = 310 N/m 400 N-m Pou Shear Values (N) VA = VB = "Intellectual Property Co and/or communi MA = MB = Republic Act A) 293 hear V s (N) -RA/3293. Any reproduele and/