Determine the total moment of the point A. 40 mm 40 mm 70 mm Y 100 mm 85 mm, 30° 900 N 260° 800 N! 25° 1000 N 65° X E (120 mm, -40 mm, 80 mm)
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- Determine the tangential rotation (in radians) at point C. Assume E=200 GPa and I=15x10^6 mm^4. P(kN)=7.5Determine the solution for the bar forces in the truss shown when P = 1 kip and x = 5 ft: AC = -1732.05 AB = 2000 BC = -866.03 BD = 2500 DC = 2020.73 EC = -3175.43From the system below, determine absolute Moment about point O. (absolute value only)
- The slotted arm OA rotates about a fixed axis through O. At the instant under consideration, θ = 32°, θ˙ = 47 deg/s, and θ¨ = 21 deg/s2. Determine the magnited of the force F applied by arm OA and the magnitude of the force N applied by the sides of the slot to the 0.3-kg slider B. Neglect all friction, and let L = 0.64 m. The motion occurs in a vertical plane.Replace the loading system by an equivalent resultant force and couple moment acting at point ?. Length AB = 1m Length BC = 2m F1 = 80 N F2 = 60 N F3 = 120 N Angle with respect to x-axis = 32 degrees Moment couple = 195 NmData are as follows: P=6.2 kN, L=3.2m, d=1.25m, b=80mm, t=25, h=120mm, h1=90mm. Determine the moment of inertia about the centroidal x-axis in mm^4.
- Rotation of bar OA is controlled by the lead screw which imparts a horizontal velocity v to collar C and causes pin P to travel along the smooth slot. Determine the values of and dot theta where r= overline OP if h = 160mm x = 120mm and v = 25mm / s at the instant represented.Determine the centroidal moment of inertia, Ixo and Iyo of the shaded figure.determine the moment forve F about point O. The force has a magnitude of 800N and coordinate direction angles of alpha=60deg, beta=120deg, and gamma=45deg. Express the result at a cartesian vector.
- Solve the following indeterminate beam by the moment distribution method. Determine the reactions and draw the bending moment diagram. (Ans : Ay=4.156, By=10.839, Cy=34.937, Dy=30.068, MAB=-0.677, MBA=17.396, MBC=-17.396, MCB=16.929, MCD=-16.929, MDC=10.285 )Determine the orientation of the main barycentric axes and the corresponding moment values of inertia of the illustrated surface (Figure 6.19) using the Mohr circle. (Are given Ix = 6.16 x 106 mm4 e Iy = 60.9 x 106 mm4 ).Moment of Inertia about the Xo axis. (Ixo)