The given cross-section represents a built-up member made of A572 Gr. 42. The section is to be used as a bending member, loaded about the horizontal axis, as shown. Please calculate the plastic moment capacity, Mp, of the beam. PL 10" x 3/4" PL 14" x 1/2" Axis of Bending PL 8" x 1" = Ai Yi Ai PL 5" x 1" = (8x1 x 1/2) + (5X1 × 5 × 2 ) + ( 14 x 1/2 × (1+1)) + 10 x 3/4 (8x1x2) + (5×1) + (14+1) + (10x314) 4 + 25+ (7*8) + (1 × 123) 16 + 5 + 7 + 15/2 15.6. Frim

The beam is made from four boards nailed together as shown below. If the nails can each support a shear force of 500 N, determine their required spacing s' and s if the beam is subjected to a shear of V = 3.5 KN. 25 mm 250 mm 250 aut BE 40 mm 25 mm 25 mm 50 mx

Q₁: Analyze the truss shown below B с <50k 3m IMI A E 100ku EA is Constant for all members + Am X Am

Rigid member ABCD shown here is used to support a 2 kN weight. This member is 6-m-long. Steel (E = 200 GPa) rods BE and CF have a diameter of 0.5 cm and length of 2 m. What is the deflection of point d when the weight is applied? (A) 4.6 mm (B) 2.3 mm (C) 3.8 mm (D) 5.5 mm +x-w

In the bridge truss shown, the end chord AB is composed of two C 230 x 30 channels latticed together so that the fabricated section has equal moments inertia about the axes of symmetry.  Properties of C 230 x 30 lx = 24.1 x106 mm4 A =3809 mm2    Compute the slenderness ratio of section AB.   Round your answer to 2 decimal places.

Compute the deformation of the beam using area method:E= 200 GPa I= 1000 x 106 mm4

A steel beam is subjected to a uniform load with length of 8m. Assume that the beam is simply supported. Use Fy= 248 Mpa. Properties of W-shape beam d=229 mm bf=210 mm rf=23.7 mm Tu-14.50 mm kdes=33. 80mm ry=53.80 mm Ix=113 x 10^6 mm^4 Iy-36.9 x 10^6 mm^4 Sx-990 x 10^3 mm^3 Zx 1150 x 10^3 mm^3 J-2100 x 10^3 mm^4 Cu-387 x 10^9 mm^6 What is the nominal shear strength capacity of the section (in kN)?

The two-dimensional framework consists of two bars CE and CD pinned at C, D and E; and a horizontal bar AB pinned at A as shown in the figure. Because of an assembly error the bar AB is slightly short of length ?. Determine the required axial force necessary to close the gap ?. All bars are made of steel and of the same cross-section and modulus of elasticity ? = 200 ??a

The truss shown is part of a roof system supporting the following service loads: = 750 Pa of Roof live load horizontal projection of the roof surface Purlin weight = 175 Pa of roof surface Roofing materials = 725 Pa of roof surface Wind load = 1,400 Pa perpendicular to roof surface Trusses are spaced at 6 m on centers and sag rods are used at midspan between trusses. Spacing of purlins is 0.7 m on centers. Use A36 steel (Fy= 250 MPa and Fu= 400 MPa). Total allowable deflection is L/240 where L is the length between supports. Consider only loads perpendicular to the strong axis in computing for the actual deflection. Consider moment, shear and deflection. For loading combinations refer to NSCP 2015. Use LRFD Tgagrod Purlin 3,5m 15m Determine the factored uniform load (KN/m) normal to the x-axis.0

A beam is built-up from the following A36 plates: 420x20 plates as flanges and 500x20 plate as web. The beam is simply-supported and subjected to concentrated load at midspan. The member is laterally supported at the ends only Limiting L Values:Lp = 4.762 mLr = 11.810 m Section Properties:A = 27200 mm2Ix = 1 370 026 667 mm4Sx = 5 269 333.333 mm3rx = 224.430 mmIy = 246 960 000 mm4Sy =  1 176 000 mm3ry = 95.286 mmJ = 3 626 666.667 mm4c = 1.0 (doubly symmetric I-shaped member)rts = 110.753 mmho = 520 mm   Compute for the ultimate moment capacity (in kN-m) of the beam if it spans 10m. Please answer this asap.for upvote.thanks