Draw the shear and moment diagrams for the shaft. Let P = 9 kN, a = 2 m, and L = 6 m. There is a thrust bearing at A and a journal bearing at B. Answer: Full solution posted on Drive B

Problem Statement Based on Problem 7-60 from the textbook. The shaft is supported by a smooth thrust bearing at A and a smooth journal bearing at B. Draw the shear and moment diagrams for the shaft. w=285 lbs/ft a=5.4ft

UPVOTE WILL BE GIVEN. WRITE THE COMPLETE SOLUTIONS. NO LONG EXPLANATION NEEDED. SOLVE IN 3 DECIMAL PLACES. CALCULATE AND DRAW THE SHEAR AND MOMENT DIAGRAM.

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W= 325 lbs/ft a= 6.8 ft

W=60lbs/ft a=7ft b=5.5 ft

Please don't provide handwritten solution.   Draw the normal, transverse and bending moment diagrams for the structure represented in the figure. could be more specific in the balance equations for each effort

Here are the dimensions, sorry for not having them earlier  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 ofn = 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.a) The aerodynamic center for problem 3 is 0.1 m from the y axis (neutral axis). Calculate thetwist angle caused by the lift force. b) For problem 3, calculate the reactions at the fixed end.  c) Assume the engine in problem 3, applies a torque around the x – axis of the spar of 100 kN-m,calculate the angular delfection of the wing at x = 3 m due to the engine.