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A single stream tube is selected to characterize the air flow past the wing of an aircraft in flight at an altitude of 20,000 ft at an airspeed of 275 ft/s. The free stream cross-sectional area of the stream tube is 0.07 ft^2. What is the airflow speed in the stream tube at a location near the wing where the cross-sectional area of the stream tube is 0.05 ft^2. What is the static pressure at this location?
the wall of a heat exchanger receives a variable heat flux as shown in the figure. the heat flux is q dot of second
the 230000 lb space shuttle orbiter touches down at about 220 mihr. at 200 mihr its drag parachute deploys. at 35 mihr
the potential at location a is 377 v. a positively charged particle is released there from rest and arrives at
a full revolution has 100 rpm flywheel rotation. the press is equipped with two hand palm buttons mounted on the machine at a distance of 20 inches from the point of operation. How many engagement points on the flywheel would be necessary to make ..
Plot the moment about B for 320mm
two processes are used to produce forgings used in an aircraft wing assembly. of 200 forgings selected from process 1
Design of absorption column and the cooler. Process design of other units should be completed along with pipe sizes.
1. a solid cube of copper with each side 1.0 ft is converted into metallic powders of spherical shape by water
the magnitude of the velocity vector of the car is v80 fts. if the vector v forms an angle theta 0.09 rad with the
natural gas at 70 f and standard atmospheric pressure of 14.7 psi is compressed isentropically to a new absolute
Air at 90 kpa and -7 C enters an adiabatic diffuser steadily with a velocity of 180 m/s and leaves with a low velocity at a pressure of 100 kpa. The exit area of the diffuser is 5 times the inlet area. Determine (a) the exit temperature and (b) th..
in figure below a charged particle moves into a region of uniform magnetic field goes through half a circle and then
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