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Design a radial plate cam to move a translating roller follower through 30 mm in 30°, dwell for 100°, fall10 mm in 10°, dwell for 20°, fall 20 mm in 20°, and dwell for the remainder. Camshaft ro = 200 rpm. Minimize the follower's peak velocity and determine the minimum prime circle radius that will give a maximum 25° pressure angle. Determine the minimum radii of curvature on the pitch curve.
A Pelton wheel turbine rotates at 240 rpm, has a pitch diameter of 3.0 m, a bucket angle of 165°, and a jet diameter of 5.0 cm. If the jet velocity at nozzle exit is 60 m/s and the relative velocity leaving the buckets is 0.9 times that at entry t..
A pipe transports water in a 4-cm-diameter pipe with an average velocity of 10 m/s. The pipe undergoes a 90 degree bend and exits out a 2-cm-diameter nozzle. Assuming no friction losses in the bend, the total force of teh water on the bend is nearest..
Evaluate the variation of hoop stresses across the wall of the compound cylinder.
at 60oc the surface of water is .0662nm and that of mercury yis .47nm. determine the capillary height changes in these
pressurized water pin 10 bar tin 110 deg c enters the bottom of an l 10-m-long vertical tube of diameter d 100 mm
a system consisting of 3 lb of water vapor in a piston-cylinder assembly initially at 350 degrees f and a volume of
Find the natural frequency of the longitudinal, the transverse, and the torsional vibration of the system.
a machinable grade of aluminum is to be milled on an nc machine with a 20 mm diameter four tooth end miling cutter
you are designing an ex vivo artificial organ. the cells in the organ cannot tolerate shear stress in excess of 0.5 gcm
refrigerant 134a is the working fluid in an organic rankine cycle. saturated vapor at 60degc enters the turbine and the
ENME352-16B: Dynamics Assignment. Using the MATLAB code given in Appendix 1, find the natural frequencies and modes. You will need to change the definition of elements of the matrices K and M
an airplane has a mass of 30mg and its engines develop a total thrust of 50kn during take-off. if the drag d exerted
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