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It is common to use double cross bracing in a steel structure so that only tension capacity is required. Consider cross bracing that might be used in the roof of a portal frame. Explain what might be the best type of member (ie what cross section shape) for effectiveness and cost, and explain why.
Efficient truck access from road to the loading docks and efficient movement of trucks on site (Note that the trucks will back up to the loading docks.)
The relative roughness ofa pipe is 0.0005, if the blasius equation is applicable for Thecflow Reynolds number above 2700 rather then 3000
49309 Quality Planning and Analysis - aim of providing students a practical case where they could apply the various quality (planning and analysis) tools
If the aircraft flies at 9000 m standard altitude, make a plot of drag (in N) versus speed (from stall to 240 m/s) and determine the optimum emise velocity (minimum drag per unit speed).
calculate the magnitude of the force on the piston pin A for the crank angle θ = 90° (Suggestion: Use the alternative moment relation, Eq. 6/3, with B as the moment center.)
A section of a road has a superelevation of .6% and a curve of 600ft radius. What speed limit will you recommend at this section of the highway
Plot the turbulence intensity profiles for the velocity components and compare the results from (c) with the actual Durst curve assuming the mean speed is like an hourly speed.
An oil spill has caused the pollution of the groundwater in a small region beneath an industrial site. How long would it take the polluted water from that location to reach a drinking water well located 100 m down gradient? Assume no retardation ..
The depth of the water in the flume is 3m. The average velocity is 1.7m/s. Compute the hydraulic energy at the surface of the water and at the bottom of the flume.
Assuming that the average stack gas velocity is 10.0m/s and the stack is circular with a 3.0 meter diameter, calculate the mass emissions rate of NO2 in kg/day.
A smart, anti armour weappon is launched of an aircraft flying at 250 knots (422 FT/s) straight and level at an altitude of 300FT above the ground, the weapon is released from the aircraft with an initial downward velocity of 15FT/s.
Assuming the flow through the nozzle to be isentropic, determine the exit area and the exit Mach number.
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