Calculate the normal stresses (in Pa) at point Bof the bracket caused by the 23010N force.
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A: P= 11633 N Width of the cross section, b= 60 mm Height of the cross section, h= 180 mm
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Q: b) For the thin walled pressure vessel subjected to an internal pressure of 150 psi and as shown…
A: Given data: - The pressure inside vessel is P = 150 psi. The length of the vessel is L ft. The…
Q: Find the principle stresses at A and maximum shear stress.
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Q: Calculate the normal stresses (in Pa) at point A of the bracket caused by the 11023N force. E4.png…
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Q: Find normal and shearing stresses at point A .
A: For the Normal Stress at pt.A (considering the maximum stress condition) Normal Stress, σx = PA…
Q: b) For the thin walled pressure vessel subjected to an internal pressure of 150 psi and as shown…
A: Given Data Internal pressure of vessel is: P=150 psi The length of the vessel is : L ft Thickness…
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A: Given: The thickness, t = 15 mm The width, b = 70 mm
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Q: Calculate the normal stresses (in Pa) at point A of the bracket caused by the 11023 N force.
A: The stress due to normal force on the beam can be determined as,
Q: 3. For the state of stress shown below, calculate the principal stresses and maximum shear stress.
A: σx = 90 Mpa σy = -60 Mpa Txy = 20 Mpa
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Q: Calculate the normal stresses (in Pa) at point A of the bracket caused by the 11023 N force. E4.png…
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Q: A state of stress at a point A is given by ox = 210 MPa, oy = -140 MPa, and txy = 95 MPa. Which of…
A: The correct answer is option e) 234.071 Mpa
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Q: Calculate the normal stresses (in Pa) at point Bof the bracket caused by the 23010N force. E4.png -…
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Q: b) For the thin walled pressure vessel subjected to an internal pressure of 150 psi and as shown…
A: Permissible stress is stress which produces due to pressure or forces which does not exceed the…
Q: For the thin-walled pressure vessel subjected to an internal pressure of 150 psi and as shown below,…
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Q: Oy = 90MPA %3D Try 60MPA %3D Ox=20MPA
A: Given Data Normal stresses σx= 20MPa σy=90MPa Shear stress fxy=60MPa Main stresses are the…
Q: A state of stress at a point A is given by ox 210 MPa, oy = -140 MPa, and txy = 95 MPa. What is the…
A: Given, σx=210 MPaσy=-140 MPaτxy=95 MPa
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Q: b) For the thin walled pressure vessel subjected to an internal pressure of 150 psi and as shown…
A: Given data: - The pressure inside vessel is P = 150 psi. The length of the vessel is L ft. The…
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Q: A state of stress at a point A is given by ax = 29 MPa, oy =- 195 MPa, and txy = -3.751 Which of the…
A: Data given- σx = 29 MPa σy = 195 MPa τxy = -3.75 MPa
Q: a) Calculate the principal stresses, given that the state of plane stress for an element is: Oy =…
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Q: C 800 mm 18 mm dia. Rectangular bar B D 16 mm thick 25 mm 400 mm A F - F -800 mm
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Q: Calculate the normal stresses (in Pa) at point Bof the bracket caused by the 25139 N force. - 540 mm…
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Q: A force 10N is applied to one end of a 10 inches diameter circular rod. Calculate the stress. 3.821…
A: Answer: The stress in the rod is 197.3525 N/m2.
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A: Given data : Stress=σ Area=A Find : Force
Ans: 11,708,888.89
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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.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.Explain the method of representing the combination of normal and shear stresses acting on any plane through an incremental element on shear stress–normal stress coordinates.
- A 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.For the two-dimensional stress fi eld shown in Fig. it isfound thatσxx = 3000 lbf/ft2 σyy = 2000 lbf/ft2σxy = 500 lbf/ft2Find the shear and normal stresses (in lbf/ft 2 ) acting onplane AA cutting through the element at a 30° angle asshown.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 plates
- A rectangular block of material is subjected to a shear stress of 30MN/m2 together with it's associated complementary shear stress. Determine the magnitude of the stresses on a plane inclined at 30 degrees to the directions of the applied stresses,which may be taken as horizontalA 60˚ strain rosette measures the following strain at a point on the aluminum skin ofan airplane. ϵ0 = 160 ×10-6 m/m, ϵ60 = -220 ×10-6 m/m and ϵ120 = 360 ×10-6 m/m. Using E = 10 ×106 psi and v = 0.3, Determine the principle stresses and the maximum in-plane shear stress.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.