Compute the moment of inertia for the built up section, shown below about the strong axis only. - ½"× 4" Web Flange Distance Area, Depth, Work- able Gage Thickness, Width, Thickness, Shape Kdes Kart in. in. in. % 152 32 in.? in. in. in. in. in. in. in. W18x71 x65 x60 x55 x50 20.9 18.5 182 0.495 2 19.1 18.4 18%0,450 h6 % 17.6 18.2 1840.415 16 4 16.2 18.1 18% 0.390 % 7.64 7%% 0.810 1/16 1.21 1½ 7.59 75% 0.750 4 1.15 1/16 8 7.56 72 0.695 W1e 1.10 1%% 13/16 16 7.53 72 0.630 1.03 1/16 13/16 13/16 14.7 18.0 18 0.355 % 16 7.50 72 0.570 % 0.972 14 W18 × 65 Compact Nom- Section inal Torsional Axis X-X Axis Y-Y Properties Criteria ho Wt. Cw by Ib/ft 24 71 4.71 32.4 1170 65 5.06 35.7 60 5.44 38.7 55 5.98 41.1 50 6.57 45.2 in. in. 127 in. in. 60.3 in. in. in. 3.49 2.73 in. in. 7.50 146 7.49 133 7.47 123 in. 15.8 1.70 24.7 2.05 17.7 14.4 1.69 22.5 2.03 17.7. 13.3 1.68 20.6 11.9 1.67 18.5 2.00 17.5 10.7 1.65 16.6 in. in. 4700 1070 117 54.8 4240 984 108 50.1 2.02 17.5 2.17 3850 98.3 7.41 112 88.9 7.38 101 890 44.9 1.66 3430 800 40.1 1.98 17.4 1.24 3040 星皇

Compute the moment of inertia for the built up section, shown below about the strong axis only. - ½"× 4" Web Flange Distance Area, Depth, Work- able Gage Thickness, Width, Thickness, Shape Kdes Kart in. in. in. % 152 32 in.? in. in. in. in. in. in. in. W18x71 x65 x60 x55 x50 20.9 18.5 182 0.495 2 19.1 18.4 18%0,450 h6 % 17.6 18.2 1840.415 16 4 16.2 18.1 18% 0.390 % 7.64 7%% 0.810 1/16 1.21 1½ 7.59 75% 0.750 4 1.15 1/16 8 7.56 72 0.695 W1e 1.10 1%% 13/16 16 7.53 72 0.630 1.03 1/16 13/16 13/16 14.7 18.0 18 0.355 % 16 7.50 72 0.570 % 0.972 14 W18 × 65 Compact Nom- Section inal Torsional Axis X-X Axis Y-Y Properties Criteria ho Wt. Cw by Ib/ft 24 71 4.71 32.4 1170 65 5.06 35.7 60 5.44 38.7 55 5.98 41.1 50 6.57 45.2 in. in. 127 in. in. 60.3 in. in. in. 3.49 2.73 in. in. 7.50 146 7.49 133 7.47 123 in. 15.8 1.70 24.7 2.05 17.7 14.4 1.69 22.5 2.03 17.7. 13.3 1.68 20.6 11.9 1.67 18.5 2.00 17.5 10.7 1.65 16.6 in. in. 4700 1070 117 54.8 4240 984 108 50.1 2.02 17.5 2.17 3850 98.3 7.41 112 88.9 7.38 101 890 44.9 1.66 3430 800 40.1 1.98 17.4 1.24 3040 星皇

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

Determine the shear strain vxy at corners A and B if the plate distorts as shown by the dashed lines. mm 2 mm 4 mm 2 mmț B 300 mm {2 mi D A 400 mm 3 mm
Convert the following and round off to nearest hundredth if necessary. 10ft³ to cm³
PLATE # 3 CALCULATE Oo AND Yo OF THE BEAM LOADED AS SHOWN USING CONJU GATE BEAM METHOD 5KN/m 20KN 30 KN M 2m 2m 2m 2m Im 21 E CONSTANT
10 GN/m² to kip/inch²
1:01 < 21_S_5_TrussDeflection... Q Structural Analysis СЕ З32 Classwork Find the vertical deflection at joint C under the loading shown. The area of all bars are the same and equal to 4 in' and E- 30,000 ksi. A is a pin and B is a roller support. 40 30 30 Figure P-3 25 Dashboard Calendar To Do Notifications Inbox
The pump in the figure discharges water at 45 lit/s. Neglecting losses and elevation changes, 3. What is the added head?
Virtual Work for Beams and Frames #2 Determine the slope and the displacement at the end C of the beam. E = 200 GPa, I = 70(10°) mmª. P = Last 2 digits of ID number a = 5th digit of ID number (max value = 3) P Use %3D 4 kN ID # = 18-2363-391 P = 91 a = 6, but use 3 (max) e.g., A C |D B- a - 3 m -3 m
100 mm → 20 mm 30 1 140 mm. Xo -20 mm Comment Q1. Determine the moments of inertia of the Z-section about its centroidal x, and yo axes. ,24 mm 1ST O Q2. Determine the location of the centroid x, y and the moments of inertia Ixx and lyy of the shapes shown below. 100 mm -100 mm- Y Le Highlight Draw 20 mm Q ет O L 12 mm TIL ⠀ 100 mm 12 mm FONA Text Fill & Sign More tools 000 000 000 i
attempt- 138326&cmid-4951 GGoogle O UVLe: Log in to the.. table 4. Which of the following shows an appropriate diagram of the tension forces acting on the ring such that it is possible for the resultant to be a zero vector? Note that the value of G is not equal to H. Hint: The eraser does not slide if the resultant of the frictional force and normal force is vertical. 5. Which of the following best approximates the value of the angle h (in degrees) if G = 100 N and H = 75 N? acer E11 NumLk Verr. Num F9 F10 F7 F8 F4 F5 F6 E3 8. 9) & 7 24 9. 6. U 4 5 0 6 P R H. 1 K 2 L G. MO CO
Q2 All members of the truss in Figure Q2 are to be fabricated from the same stock of thin-walled, round, steel tubing. Two external loads are exerted at the edge of lower part of member BF and CE with magnitudes of 10kN and 15KN, respectively. The loads are placed in a vertical position abiding gravitational direction. Analyse the truss structures based on the instruction listed. (i) Among all rods of the truss shown in the figure, there is a member that supports no loading known as a zero-force member. Figure out the member(s) with solid justification. (ii) The truss is supported with two surface forces as shown. Determine the magnitude and direction for each support reaction. (iii) Determine the axial stress in all rods of the truss by mentioning either the rod is experiencing compression or tension.
3. Determine the moment of inertia with respected to 25 mm x- (horizontal) and y- (vertical) axis through the centroid of the two 250 x 25 mm steel plates and two C381 x 74 channels that are welded together 254 mm C381 x74 to form the cross section shown in Figure 3. 25 mm 250 mm- Axis XX Axis YY Flange Thicknesu Wob Thickness Arca mm2 Depth Wid th 108 mmt Shape C381 x 71 105 mmt 1.58 mm mm mm mm mm mm 9485 381 91.4 165 18.2 168 133 22.0 20.3
Y Given: X x1 x2 . x1 = 15.35 mm • x2 = 16.74 mm . x3 = 16.10 mm .y1 = 19.32 mm y2 = 20.55 mm y3 = 16.37 mm mie x3 sterren T y3 y2 y1 Find x & y centroid