Determine the length L of the center portion of the bar as shown on Figure Q3 so that the maximum bending stress at A, B, and C is the same. The bar has a thickness of 10 mm.
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- The aluminum machine part is subjected to a moment of M=95 N-m. (Figure 1) 10 mm 10 mm 10 mm 40 mm 20 mm 20 mm 10 mm 10 mm A Determine the maximum tensile bending stresses in the part. Determine the maximum compressive bending stresses in the part.6 kN/m 4 kN/m 1.5 m- What is the concentrated load of the rectangular loading as shown in the figure? 6 KN 2.5 KN 8 KN 4.5 KNThe shaft is supported at its ends by two bearings AA and BB and is subjected to the forces applied to the pulleys fixed to the shaft. (Figure 1) The T1=T1= 585-NN forces act in the -zz direction and the 200-NN and 80-NN forces act in the +yy direction. The journal bearings at AA and BB exert only yy and zz components of force on the shaft. Part A Determine the resultant normal force on the cross section at CC. Express your answer to three significant figures and include appropriate units. NC= values ? NC= units? Determine the resultant shear force in the yy direction on the cross section at CC . Express your answer to three significant figures and include appropriate units. (VC)y Values ? (VC)y units ?
- Question 4: Two wrenches are used to tighten the pipe. If the pipe is made from a material having an allowable shear stress of Tallow = 85 MPa, check the allowable force for external and internal diameter of pipe and determine the allowable maximum force P that can be applied to each wrench. The pipe has an outer diameter of 25 mm and inner diameter of 20 mm. 250 mm B 250 mm Figure 4 Answer: Torque = 0.5P, Polar moment of inertial J = 2.26 x 108 m4, outer diameter PS %3D 307.36N, inner diameter P S 384.2 N, Pallowable = 307.36NGiven the following figure, answer the following multiple choice question 1) If loadings on the bar are to be replaced by an equivalent single force, R, acting along segment AB, which of the following best gives the magnitude and location of this force R? A. R = 2kN down, 9.9m to the right of A B. R = 8kN down 7.73m to the right of A C. R = 2kN down 46.1m to the right of A D. R = 8kN down 19.6m to the right of AShow the zero force members on the figure (label them on the figure and list them on the side). (Note: you don't have to solve the entire structure) D E 60 kips В F A M L K J G Н 180 kips 120 kips
- 1. A circular shaft with a keyway can be approximated by the section shown in Fig. r=b Ay r r=2acose Figure 1: Circular shaft with a keyway. The keyway is represented by the boundary equation r = b and the shaft is represented by the boundary equation r = 2a cos 0. Show that using a Prandtl stress function of the form ²) (₁ (1-2a cos) X v = K (b² − ²) (1 – : will solve the problem of torsion on this shaft and find the constant K (assume an applied torque T). Compute the shear stress components Txz and Tyz. (Hint: start by converting the stress function to Cartesian coordinates).Direct a key d the Hub Shear plane Hub Key F2 y, or anical F1 T=Torque Shaft T=F(D/2) F = Force of shaft on key F= Force of hub on key Side view -D Shaft diameter End view Shear Shaft plane Hub F1 Key F2 Shear area = A, = bxL %3D Enlarged view of key Pictorial sketch of key, shaft, and hub НоуThe shaft is supported at its ends by two bearings A and B and is subjected to the forces applied to the pulleys fixed to the shaft. ( Figure 1) The T₁ = 410-N forces act in the -z direction and the 200-N and 80-N forces act in the +y direction. The journal bearings at A and B exert only y and z components of force on the shaft. Figure X 200 mm 300 mm 150 mm 150 mm 200 mm D 400 mm B 200 N 200 N Z 80 N 80 N 1 of 1 > ▾ Part B ▾ Determine the resultant shear force in the y direction on the cross section at C. Express your answer to three significant figures and include appropriate units. (Vc), = 245.71 ▾ Part C Submit Previous Answers Request Answer * Incorrect; Try Again; 4 attempts remaining Submit (Vc), = Value Part D Determine the resultant shear force in the direction on the cross section at C. Express your answer to three significant figures and include appropriate units. T= HA Submit Part E ריהם Determine the resultant torque on the cross section at C Express your answer to three…
- 3. Four pulleys are attached to the 50-mm-diameter aluminum shaft. If torques are applied to the pulleys as shown in the figure, determine the maximum shear stress in each segment and the angle of rotation of pulley D relative to pulley A. Use G = 28 GPa for aluminum. a. Tab= b. Tbc= C. Tbc= ad= 1100 N·m 800 N·m D C 900 N·m 600 N m B A 2 m3 m2 mQuestion 2) arm of Figure B from point x z plane, a horizontal angle of θ = 44 ° angled F = 26 kN size and a force C at the point z in the direction of M = 18 kn.m acts a moment in size. The lengths of the arm are also given as L 1 = 1.6 m and L 2 = 1.3 m . It is desired to determine the stress state of point A on the aa section taken from the arm. The radius r of the section is r=0.029 m and the shear modulus of the sleeve material is also G = 79 Gpa . According to this; Question 2-C) Find the normal stress caused by the normal force at point A ( Write your result in MPa .) Question 2-D) Find the normal stress caused by the bending moment at point A. (Your result MPa in the size of your font.)Question 2) arm of Figure B from point x z plane, a horizontal angle of θ = 44 ° angled F = 26 kN size and a force C at the point z in the direction of M = 18 kn.m acts a moment in size. The lengths of the arm are also given as L 1 = 1.6 m and L 2 = 1.3 m . It is desired to determine the stress state of point A on the aa section taken from the arm. The radius r of the section is r=0.029 m and the shear modulus of the sleeve material is also G = 79 Gpa . According to this; Question 2-A) Find the shear stress at point A due to the shear force . ( Write your result in MPa .) Question 2-B) Find the shear stress due to the torsional moment at point A. ( Write your result in MPa .) Question 2-C) Find the normal stress caused by the normal force at point A ( Write your result in MPa .) Question 2-D) Find the normal stress caused by the bending moment at point A. (Your result MPa in the size of your font.)