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You are designing a converging-diverging nozzle to operate at sea level. The nozzle will be mounted on a glider that flies at 60 mph. The entrance to the nozzle is 1 m^2. What is the stagnation pressure and Mach number of flow entering nozzle? What should throat and exit area be if exit mach number is 2?
consider the function fxx3-2x4 on the interval -22 with h0.25. use the forward backward and centered finite difference
what happens if a positive edge dislocation meets a negative edge dislocation on the same slip plane with a parallel
a small spherical ball is gently released from rest in a cylindrical tank completely filled with glycerine. the ball
find the isentropic and the second law efficiencies for a turbine. it receives steam at 3000 kpa 500c and has two exit
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the launch vehicle takes the moon orbiter to a circular orbit around the earth at 300km altitude. the orbiter is to
a gas refrigeration cycle with a pressure ratio of 3 uses helium as the working fluid. the temperature of teh helium is
1. determine the solar elevation at solar noon for winer solstice equinox and summer solstice for elevations 30 40 and
consider a brayton cycle with the following given data pressure ratio 9.2 air at compressor inlet is at 25 deg f air
a link AC has uniform rectangular cross section 3mm thick and 25mm wide. Determine the normal stress in the central portion of that link? solution
sun a 5800 k transfers heat to earth at an average rate of 1360 w per m2 of surface area of earth. the earth has a
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