PROBLEM 2 Determine the slope of end A of the cantilevered beam. E-200 GPa and 65x106...
E- 230 GPa and I 65.0(106) mm1 (Figure 1) Part A Determine the slope of end A of the cantilevered beam. Express your answer to three significant figures and include the appropriate units Value Units Submit Request Answer Provide Feedback Next > Figure 1 of 1 10 kN 3 kN/m
4. Determine the slope and deflection at end point C of the cantilever beam shown in the figure. Use E = 200 GPa, I = 10 x 106 mm 3 kN/m 2 kN.m A B 2 m 2 m
B-220 GPa and I - 650(109) mm (Figure 1) Part A Determine the slope of end of the cantilevered beam Express your answer to three significant figures and include the appropriate units. | HÁ ? Figure 1 of 1 > Value Units 10 KN 3 N/m Submit Previous Answers Request Answer * Incorrect; Try Again; 3 attempts remaining Provide Feedback
Q-3 For the beam and loading shown, determine (a) the slope at end A, (b) the deflection at point C. Use E = 200 GPa. I r 6.87, io'--' · '.g7s/o''-, 20 kN 12 kN/ w150 × 13.5 0.8 m 0.4 m im
E = 180 GPa and I = 65.0(106) mm. 10 KN 3 kN/m -3 m Part A Determine the slope of end A of the cantilevered beam. Express your answer to three significant figures and include the appropriate units. H ? 5.10-5
Determine the slope at A of the overhang beam. E = 200 GPa and I = 40.7(106)mm4Express your answer with the appropriate units.
Determine the slope at A of the overhang beam. E = 200 GPa and I = 48.6 (106) mm4 (Figure 1)
Problem 3: For the beam shown find the slope and deflection at point B and C 100 KN 300 kN-m 6 m E = constant = 70 GPa 1 = 500 (106) mm Problem 4: For the beam shown find the deflection at point B and the slope at point A 80 KN 12 m 12 m E = constant = 200 GPa I = 600 (106) mm
2. For the beam and loading shown, determine the slope and deflection at point B. Where: w = 2 kN/m, L = 2 m, E = 200 GPa, and I = 1.708 x 10 m. B 1/2- 1/2
2. Consider a cantilevered beam with length L = 3 m, uniform E = 180 GPa, Iz- 5.375 × 10-8 m. and ρ 3.0 kg/m. (a) (20 points) Compute, by hand, the first 5 (lowest) natural frequencies for this beam. Note, unlike for the simply-supported beam problem, you will not be able to solve, analytically, the transcendental equation obtained from the application of the boundary conditions to the general free vibration solution. So, use Matlab roots of this equation numerically