The figure shows the cross-section of a beam that is composed of a wide-flanged structural profile, whose specification is indicated in the figure, and two steel plates, joined by means of screws, placed in pairs with a longitudinal separation of 20 cm . If the beam is subjected to a vertical shear force of 25 KN, determine the shear stress supported by each bolt in the topsheet. Please add the free diagram bo

consider a beam with two 60-inch-long rods. The rods have a cross section area of 0.50 in 2 . Find the axial stress in each rod, draw the shear and moment diagrams for the beam, and find the maximum stress in the beam.

Determine the shear force acting at each of the following locations:(a) x = 0+ ft (i.e., just to the right of support A)(b) x = 9 ft(c) x = 12.333333333333 ftWhen entering your answers, use the shear force sign convention.Answer:(a) V =  kips.(b) V =  kips.(c) V =  kips. The shear-force diagram crosses the V = 0 axis between points A and B. Determine the location x where V = 0 kips.Answer: x = Enter your answer in accordance to the question statement ft. Determine the maximum bending moment that acts anywhere in the beam. When entering your answer, use the bending moment sign convention.Answer: Mmax = Enter your answer in accordance to the question statement kip-ft. Use the graphical method to determine the bending moment acting at each of the following locations:(a) x = 3.3 ft(b) x = 9 ft(c) x = 12.6 ftWhen entering your answers, use the bending moment sign convention.Answers:(a) M =  kip-ft.(b) M =  kip-ft.(c) M =  kip-ft.

A wide flange beam as shown below is subjected to a shear force V. Using the dimensions of the cross section, determine the following quantities: a. τmax in the webb. τmin in the webc. τmax/ τaverage of the web

The internal shear force V at a certain section of an aluminum beam is 8.7 kN. If the beam has the cross section shown (assume a=44 mm, b=87 mm, tw=t=4 mm, d=88 mm), determine: (a) the shear stress ty at point H, which is located 44 mm above the bottom surface of the tee shape. (b) the maximum horizontal shear stress Tmax in the tee shape. bf H a Answers: (а) тн — i MPa. (Б) тmах — i MРа.

Determine the axial force, shear force, and bending moment at point J located on member AB of the landing gear of an airplane, as shown in the figure.All distances are in inches.

A hemp rope L=12 m long and d=42 mm in diameter is supported from one of the roof beams in a gymnasium. Three gymnasts climb this rope together. The lead gymnast has a mass of m1=50 kg, the next gymnast has mass m2=75 kg, and the trailing gymnast has mass m3=50 kg. Determine the maximum stress in the rope (omax), and the stress in the rope at a location between the intermediate and trailing gymanst (023).

Answer the attached file

A simply supported beam (i.e., with a pin support at point A and a roller support at point D) is subjected to the external loadings shown in the figure. The cross- soction is shown to the right of the beam. 10 IN 10 KN mm 10mm Determine the shear stress developed in the cross-section n-n at point E on the web, 2m S0mm

The simply supported beam shown supports a uniformly distributed load of w = 50 kN/m. Assume x = 1.6 m, a = 3.5 m, b = 6.0 m, xk = 2.5 m. The cross-sectional dimensions of the beam are b₁ = 305 mm, t₁ = 23 mm, d = 480 mm, tw = 14 mm, and y = 85 mm. Determine the principal stresses and the maximum shear stress acting at point H. On a piece of paper, show these stresses on an appropriate sketch. ΧΗ พ bf H H B K Ун XK Ук b K a tw d