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At rated thrust, a liquid-fueled rocket motor consumes 180 lbm/s of nitric acid as oxidizer and 70 lbm/s of aniline as fuel. Flow leaves axially at 6000 ft/s relative to the nozzle and at 16.5 psia. The nozzle exit diameter is D = 2 ft. Calculate the thrust produced by the motor on a test standard sea-level pressure draw the rocket horizontally such that the direction of motion is to the right. Let the positive x-axis point to the left).
consider a mass going through a polytropic process where pressure is directly proportional to volume n-1 the process
for the following calculations take g 9.8ms2 and pwater1000kgm31. assuming there are both a pressure gage and a
tarzan king of the jungle mass 66.2 kg grabs a vine of length 14.6 m hanging from a tree branch. the angle of the vine
a hollow spherical iron container whose outer diameter is 20 cm and the thickness is 0.4 cm is filled with ice water at
Determine the tensions developed in wires , and and the angle required for equilibrium of the 30-lb cylinder E and the 60-lb cylinder F.
plot your results determined in the previous part. (c) Calculate the values of n and C in the Taylor equation solving simultaneous equations.
what fraction n of the weight of the jet airplane is the net thrustnozzle thrust t minus air resistance r required for
natural gas methane flows from a 33-in diameter gas main through a 1-in-diameter pipe and into the burner of a furnace
1 a 10-cm long and 20-cm wide circuit board is covered with 100 closely spaced chips each generating heat at a rate of
a storage tank is 40 feet above a river. water is pumped from the river to the storage tank at a rate of 0.095m3s. the
air enters the compressor of a regenerative gas-turbine engine at 300 k and 100 kpa where it is compressed to 800 kpa
at a surface cutting speed of 190 mmin the productive tool life was 60 minutes. at a surface cutting speed of 225 mmin
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