Two portions of member AB are glued together along a plane forming an angle θ with the horizontal. Knowing that the ultimate stress for the glued joint is 2.5 ksi in tension and 1.3 ksi in shear, determine the range of values of θ for which the factor of safety of the members is at least 3.0. Two portions of member AB are glued together along a plane forming an angle with the horizontal.Knowing that the ultimate stress for the glued joint is 2.5 ksi in tension and 1.3 ksi in shear, determine therange of values of 0 for which the factor of safety of the members is at least 3.0.2.4 kips02.0 in.B•

To find the range of the value of θ in the given setup Given Data Cross sectional area of the…

Two portions of member AB are glued together along a plane forming an angle with the horizontal. Knowing that the ultimate stress for the glued joint is 2.5 ksi in tension and 1.3 ksi in shear, determine the range of values of 0 for which the factor of safety of the members is at least 3.0. 2.4 kips 2.0 in. |° < 0 <| -1.25 in.

Two portions of member AB are glued together along a plane forming an angle with the horizontal. Knowing that the ultimate stress for the glued joint is 2.5 ksi in tension and 1.3 ksi in shear, determine the range of values of 0 for which the factor of safety of the members is at least 3.0. 2.4 kips 2.0 in. |° < 0 <| -1.25 in.

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

For the beam showna. Determine the maximum flexural stressb. If the nails shown in the cross-section can each support a shear force of 600 N,determine their required spacing along the beam. P=10kN Wo=8kN/m a=10m
the bars and truss have a cross section of 250mm^2. If thr maximum average axial stress in any bar is not to exceed 250N/mm^2, determine the magnitude of P of the loads that can be applied 2P 3m 3m -O E 2m B
Three plates are welded together to form the section shown. Dimensions of the cross section are b = 4.7 in., d = 14.1 in., a = 3.7 in., and t= 0.8 in. For a vertical shear force of V = 46 kips, determine the shear flow through the welded surface at B. d В b. Answer: kip/in.
2. For each of the plane stress states listed below find the three principle stresses and the maximum shear stress. a) ox 20kpsi, oy--15kpsi, Txy=8kpsi cw b) ox= 16kpsi, oy-10kpsi, Txy=5kpsi ccw c) ox= 10kpsi, oy=24kpsi, Txy=6kpsi ccw
The bars of the truss each have a cross-sectional area of 1.92 in². Determine the average normal stress in ksi in member BD due to the loading P = 10 kips. NOTE: use absolute value for Normal stress. The final answer should have 2 decimal places where: L1 =3.8 ft. L2 = 4.3 ft. B L1 D L2 E 0.75 P L2
Part 2,3,4
0.13
A pin-connected truss is loaded and supported as shown. Each aluminum member has a cross-sectional area of A= 2.9 in.2. Assume a = 3.50 ft and b=4.20 ft. If the normal stress in each member must not exceed 25 ksi, determine the maximum load Pmax that may be supported by the structure. D Answer: Pmax= i b B b kips
For the plane truss shown below loaded with a 200 kN force, determine the amount of deformation in membes (AB) & (AD) if their cross- sectional areas are known to be AB= 2500 mm² & AAD = 2000 mm² (assume E 200 GPa) 4 m B D 200 KN 2.5 m
2. The major and minor principal stresses at the point are 3 MPa and -3 MPa respectively. The maximum shear stress at the point is (A) Zero (C) 6 MPa (B) 3 MPa (D) 9 MPa
Three plates are welded together to form the section shown. Dimensions of the cross section are b= 4.7 in., d = 14.1 in., a = 2.8 in., and t= 0.5 in. For a vertical shear force of V = 42 kips, determine the shear flow through the welded surface at B. B a b Answer: kip/in.
The compound shaft is attached to a rigid wall at each end. For the bronze segment AB, the diameter is 75 mm and G = 35 GPa. For the steel segment BC, the diameter is 50 mm and G = 83 GPa. Given that a = 2 m and b = 1.5 m, compute the largest torqueT that can be applied as shown in the figure if the maximum shear stress is limited to 60 MPa in the bronze and 80 MPa in the steel. 75 mm 50 mm A Bronze B Steel