Fig. P3.29
3.29 While the exact distribution of the shearing stresses in a hollow-cylindrical shaft is as shown in Fig. P3.29a, an approximate value can be obtained for
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- A two celled tube with wall thickness 0.5 mm is subjected to a torque of 10 N.m as shown in Fig.(4). The resulting shear flows in two shells are shown below 50mm a. 9₁ +92 = 2000N/m b. 91 - 92 = 2000N/m 91 c. 291 +92 = 2000N/m d. q1 + 2q2 = 2000N/m Fig. (4) 92 50mm 50mmarrow_forward3.13 The torques T and 2T are carried by a shaft consisting of steel and aluminum segments. If the working shear stresses are 14 000 psi for steel and 7500 psi for aluminum, and the angle of rotation at the free end must not exceed 8, find the largest allowable value of T. For steel, use G = 12 x10^6 psi, and for aluminum, use G = 4 x10^6psi. T Aluminum 1.5 in.- 27/ Steel 2 in. + گری برای Happy 2 ft 3 ft as 3.14 T angle showrarrow_forwardProblem 3.15. A hollow aluminium tube of rectangular cross- section as shown in Fig. 3·27 is subjected to a torque of 56-5 kN.m along its longitudinal axis. Determine the shearing stresses and the angle of twist. Assume G = 28 GPa. 0.5m t2 = 0.006 0.25m t₁ = 0.012 0.01 (a) h t4=0.006 h = ti 13 (b) Membrane surface Fig. 3.27.arrow_forward
- 3.44 An aluminum tube with the hexagonal cross section shown is 2.5 ft long and has a constant wall thickness of 0.080 in. Find (a) the largest torque that the tube can carry if the shear stress is limited to 7200 psi; and (b) the angle of twist caused by this torque. Use G 4 x 10 psi for aluminum. -15 in - 0.075 in FIG. P3.44arrow_forwardPin Fig. 4.21 Find the minimum size of a hole that can be punched in a 20 mm thick mild steel plate having an ultimate shear strength of 300 N/mm. The maximum permissible compressive stress in the punch material is 1200 N/mm. [Ans. 20 mm]arrow_forwardQuestion 3 The tubular drive shaft for the propeller of a hovercraft is 6 m long. At full speed and power, the torque developed in the shaft is 160 kN·m. The shear modulus (G) of the shaft material is 75 GPa, and the maximum allowable shear stress is 90 MPa. (a) Determine the required inner diameter, given that the outer diameter is 250 mm. (b) What is the shear stress developed at a point in the cross-section of the shaft that is 15 mm radially inward from the outer surface? (c) What is the angle of twist of the shaft when it is operating at full speed and power? (d) If a solid shaft was used instead, what would be the required shaft diameter? (e) Given that the density of the shaft material is 7.86 g/cm³, determine the percentage weight saving achieved by using a tubular shaft as compared to a solid one.arrow_forward
- Ex. 5.4 The stresses acting on an element of a loaded body are shown below. Apply Mohr's circle to determine the normal and shear stresses acting on a plane defined by 0 = 30°. Sol. YA 30° 14 MPa -28 MPaarrow_forwardIn problem 3.52, consider the following: Do not change the total distance between points A and C. Is it possible tomove the coupling disk (point B) somewhere between A and C so that the maximum shear stresses in shafts ABand BC are equal? Explain your work concisely and in detail. Clearly and carefully draw your final designarrow_forwardOne motor delivers 100 hp to a 3-inch shaft that rotates at 210 rpm. The pulleys take 50 hp, 30 hp, and 20 hp at B, C, and D, respectively. Determine the constant stresses in the three shafts and the angle of twist of end D with respect to A, in Fig. p3.64arrow_forward
- Show the complete process and free body diagram to get the answer below.arrow_forwardSeveral forces (F = 200 N and P = 150 N) are applied to the pipe assembly as shown in Figure Q1(b). Knowing that the inner and outer diameters of the pipe are equal to 40 mm and 45 mm, respectively, determine: a) the principal planes and the principal stresses at point H located at the top of the outside surface of the pipe and sketch the orientation of the element, b) the maximum in-plane shearing stress at the same point and sketch the orientation of the element c) the absolute maximum shearing stress at the same pointarrow_forwardQ4 Direct stresses of 160N/mm2 tensile and 120 N/mm2 compressive exist on two perpendicular planes at a certain point in a body. They are also accompanied by shear stresses on the planes. The greatest principal stress at the point due to these is 200 N/mm2. What must be the magnitude of the shearing stresses on the two planes? What will be the maximum shearing stress at the point?arrow_forward
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