A cylindrical test specimen is subjected to a torsional moment of 204,520 lb-in and an axial tensile force of 155,791 lb. The specimen has a diameter of 4.9 in. Determine the torsional shear stress (psi) for the test specimen.
A cylindrical test specimen is subjected to a torsional moment of 204,520 lb-in and an axial...
A cylindrical test specimen is subjected to a torque of 5000 lb-in and an axial tensile force of 12,000 lb. The specimen has a diameter of 3 in. Determine the torsional shear stress, τ, and normal axial stress, σ, for the test specimen.
The flanged member shown below is subjected to an internal axial force of P = 6500 lb, an internal shear force of V = 4500 lb, and an internal bending moment of M = 19200 lb-ft, acting in the directions shown. d M Iw y HI a y Ilk thu The dimensions of the cross section are: bf = 8.0 in. tp = 0.61 in. d = 11.0 in. tw = 0.38 in. The cross-sectional area of the flanged shape...
The specimen failed the tensile test at an angle of 52 ° under an axial load of 100 kN. If the specimen diameter is 12 mm, determine the average shear stress and the average normal stress acting on the inclined fault plane area. If the material used for the specimen is an abnt 3140 (cr = ni) te = 650 Mpa steel would it fail?
df 1n mon diame ss: F size 0.70 V): A cold drawn C-1025 steel rod of circular cross section is subjected to a variable bending moment of 10,000 in-lb to 17,000 in-lb, as the axial load varies from-2,000 lb to 5,000 lb. The maximum bending moment occurs at the same instant that the axial load is maximum. Determine the required diameter of the rod for a factor of safety N-2.3? The steel rod is connected to the support which causes...
1. (15 points) The thin-walled pipe has an inner diameter of 0.5 in. and a thickness of 0.025 in. If it is subjected to an internal pressure of 200 psi and the axial tension and torsional loadings as shown, determine the state of stress at point A and sketch these stresses on element A. Extra Credit: What is the maximum in-plane shear stress in this element? 00 lb 100 lb 20 lb.ft 20 lb.ft
UL INTERNATIONAL UNIVERSITY LIAISON INDONESIA QUIZ 2 Il Stress- Strain calculation A cylindrical specimen of a hypothetical metal alloy is stressed in tension. Its Formula original diameter is 20mim and final diameter after tensile is 19.985 mm and its Tensile stress: final length is 84.7005 its modulus of elastic is 208 GPa, and shear modulus is 79 GPa. ava Am cross sectional area Shear stress Compute its original length and the force if the deformation is totally elastic
P B A pressurized cylindrical air tank is subjected to a force P at a collar B. The tank has an inner diameter (d = 160 mm) with wall thickness (1 = 6 mm). The gage pressure inside the tank is p = 5 MPa and the applied force is P = 9.5 kN. (a) Determine the maximum tensile stress o [MPa), maximum compressive stress oc [MPa] and maximum shear stress imax [MPa) at point a. (b) Repeat part (a)...
P Problem 3 (30 pts): Combined Loading A pressurized cylindrical air tank is subjected to a force P at a collar B. The tank has an inner diameter (d= 160 mm) with wall thickness (t = 6 mm). The gage pressure inside the tank is p = 5 MPa and the applied force is P=9.5 kN. B 450 mm (a) Determine the maximum tensile stress 0 [MPa], maximum compressive stress oc [MPa] and maximum shear stress Tmax [MPa] at point...
The cylinder with a diameter of 100 mm shown below is subjected to the an axial force F = 700 kN and a torsional moment M = 6 kN ∙ m. Given that the yielding stress of the cylinder [σ] = 140MPa ⑴ Please draw the stress state diagram of the surface points of the cylinder with concrete stress value. ⑵ And use the maximum distortion – energy criterion to judge whether the cylinder will fail or not. P. S....
P B Problem 3 (30 pts): Combined Loading A pressurized cylindrical air tank is subjected to a force Pat a collar B. The tank has an inner diameter (d = 160 mm) with wall thickness (t = 6 mm). The gage pressure inside the tank is p = 5 MPa and the applied force is P=9.5 kN. (a) Determine the maximum tensile stress o [MPa], maximum compressive stress oc [MPa] and maximum shear stress Tmax [MPa] at point a. (b)...