Calculate the normal stresses (in Pa) at point A of the bracket caused by the 11023N force. E4.png 540 mm 180 mm 180 mm 60 mm → - 4 3,
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- A cylindrical storage tank contains liquefied propane under a pressure of 1.5 MPa (gage pressure P=1.5 MPa) and is subjected to an axial force F=60 kN. Knowing that the tank has an inner diameter of 320 mm and a wall thickness of 3 mm, find the principal stresses and determine the maximum shear stress.A rubber bolt is inflated to apressure of 65kPa. At that pressure, te diameter ofthe ball is 240mm and the wall thickness is 1.25mm. The rubber has a modulus ofElasticity = 3.7 MPa and Poisson’s ratio v=0.48. Determine the maximum stress in theball if its stress is half that of the cylinder.Determine the principal stresses, the maximum in-plane shear stress, and average normal stress. Specify the orientation of the element in each case.
- Determine the stresses at points A and B as a results of applying each of the following internal loads N = 300 N, V = 250 N, M = 120 N.m and T = 300 N/m. The diameter is 20 mm. You must show your detailed solutionsA thin-walled pressure vessel is made of steel with a thickness of 2 mm and an internal diameterof 300 mm. It is subjected to an internal pressure of 10 MPa. Determine the hoop stress andlongitudinal stress developed in the vessel.A cylindrical propane tank has an outside diameter of 3.25 m. If the allowable hoop stress is 100 MPa and the allowable axial or longitudinal stress is 45 MPa, determine the minimum thickness of the pipe when the internal pressure that can be applied to the tank is 1.25 MPa.
- A 14 mm diameter rivet joins the plates that are each 1.10 m wide. The allowable stresses are 120 000 KPa for bearing in the plate material and 60 000 KPa for shearing rivet. Determine the minimum thickness of each plate and the largest average tensile stress in the platesDetermine the principal stresses andmaximum in-plane shear stress of given stresselement.The inner diameter of the AB compressed air tank is 160, the wall thickness is 1.Since the manometer pressure in the tank is 1,6 ,at point a at the top of the tank maximum normal stress and determine the maximum plane shear stress.(c=16 , d=38, e =32, g=160, h=1, k =1.6 , F=160)
- The cross-sectional area of bar ABCD is 600 mm2. Determine the maximum normal stress in the bar.The principal strains at a point on the aluminum fuselage of a jet aircraft are P1 = 780(10-6) and P2 = 400(10-6). Determine the associated principal stresses at the point in the same plane. Eal = 10(103) ksi, nal = 0.33.The yield stress for a zirconium-magnesium alloy is sY = 15.3 ksi. If a machine part is made of this material and a critical point in the material is subjected to in-plane principal stresses s1 and s2 = -0.5s1, determine the magnitude of s1 that will cause yielding according to the maximum shear stress theory.