Find the extremities that the slider A will move in left and right, and its Stroke length. АВ %3D 90 mm AC = 600 mm %3D a = 100 degrees a В
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Q: Q1) the torque on the crankshaft of engine is given by : T(N.m) = 25320 + 12600sin20 – 15650cos20…
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- Please help :( given: T(sub B) = 80.11, T = 5.67 kN-m3) The force, FT = 1 kN, and moment, MT = 0.5 kN-m, at the tip are caused by a wing tip vortexand a winglet, not shown. L = 12 m and the spar has an elastic modulus of E = 70 GPa and aPoisson’s ratio of n = 0.33. The mass of the wing is 4000 kg, and the weight of the engine is 107kN. Use 9.8 m/s 2 for the acceleration due to gravity.Consider the cross-section shown (you can look these up). Pay attention to the coordinate systemgiven in the drawing.d) where is the centroid?e) what is the area?f) Calculate the shear modulus3) The force, FT = 1 kN, and moment, MT = 0.5 kN-m, at the tip are caused by a wing tip vortexand a winglet, not shown. L = 12 m and the spar has an elastic modulus of E = 70 GPa and aPoisson’s ratio of n = 0.33. The mass of the wing is 4000 kg, and the weight of the engine is 107kN. Use 9.8 m/s 2 for the acceleration due to gravity.Consider the cross-section shown (you can look these up). Pay attention to the coordinate systemgiven in the drawing.g) Compute each of these moments of inertia with the values b = 0.4 m, d =0.5 m , t =0.1 m.
- 3) The force, FT = 1 kN, and moment, MT = 0.5 kN-m, at the tip are caused by a wing tip vortexand a winglet, not shown. L = 12 m and the spar has an elastic modulus of E = 70 GPa and aPoisson’s ratio of n = 0.33. The mass of the wing is 4000 kg, and the weight of the engine is 107kN. Use 9.8 m/s 2 for the acceleration due to gravity.Consider the cross-section shown (you can look these up). Pay attention to the coordinate systemgiven in the drawing.a) what is the moment of inertia about y-axis in terms of the symbolic dimensions shown?b) what is the moment of inertia about z-axis in terms of the symbolic dimensions shown?c) what is the polar moment of inertia in terms of the symbolic dimensions shown (i.e.about the x-axis)?d) where is the centroid?e) what is the area?f) Calculate the shear modulusg) Compute each of these moments of inertia with the values b = 0.4 m, d =0.5 m , t =0.1 m.Determine the absolute maximum shear stress in the shaft of ProblemPlease show that the Helix curve (threaded spring) r (t) = (cost, sin t, t) is constant.Is it the same as the curvature radius of the curve XY level projection (= unit circle)?
- A thin rim1.6 m external diameter is 160 mm wide and 12 mm thick. It is made in two halves with the joint parallel to the axis, and fastened together by three bolts on each side of each joint. If the maximum allowable shear stress in the bolts is 16 MPa. Determine for a speed of 500 rev/min : a) The centrifugal stress in the rim . assume = 7.8 Mg/m3 b) a suitable diameter for the bolts, if they are in single shear.A hollow shaft for a rotary compressor is to be designed to transmit a maximum torque of 4750 N-m.The shear stress in the shaft is limited to 50 MPa. Determine the inside and outside diameters of theshaft, if the ratio of the inside to the outside diameter is 0.4. [Ans. 35 mm ; 90 mm]Sketch shear flow diagram and locate position of shear center for V = 10R (N) acting downwards. Assume uniform thickness of R/360 (mm) for all segments of section shown below. Perform neat and detailed calculations using appropriate value of R given below Note R=993