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A flat plate separates two supersonic air flows. The flow along the upper surface has a Mach number of 1.4 and a stagnation pressure of 55.3 psia. The flow along the lower surface has a Mach number of 3.5 and a stagnation pressure of 316psia. At the end of the plate, the flows come together and must adjust themselves. Calculate the flow field downstream of the plate, i.e. determine the Mach number, static pressure, and flow direction for each region behind the plate.
a 20-cm-long cylindrical graphite pure carbon rod is inserted into an oxidizing atmosphere at 1145 k and 1.013105 pa
1 initially an insulated rigid tank contains 2.85 kg of water at 263oc and 1 mpa. a heater in the wall of the tank
for the fluid power system shown in figure determine the external load f that the hydraulic cylinder can sustain while
1-kg of air at 200 kpa and 127 deg c is contained in a piston-cylinder device. air is now allowed to expand in a
A Pitot-static probe connected to a water manometer is used to measure the velocity of air. If the de?ection (thevertical distance between the ?uid levels in the two arms) is 7.3 cm, determine the air velocity. Take the density of air to be 1.25 k..
consider a steam turbine in which steam enters at 10.45 mpa and 780k with a flow rate of 38.739 kgs. a portion of the
a water tank with an open top and square horizontal cross-section is to have a capacity of 5 m2. find the minimum cost
a pressized tank contains a fluid with a dinsity of 900 kgm3. the absolute pressure of the air above the fluid is p400
when the hydrofoil shown was tested the minimum pressure on the surface of the foil was found to be 70 kpa absolute
a cannonball with mass m is fired with an initial speed v0 at an angle theta ablve the horizontal. compute the time it
a frictionless piston cylinder device with a set of stops contains .5m3 of saturated h2o vapor at 200 kpa. at this
IN FE analysis, What is effect of modeling a plane stress as plane strain and vice a versa?
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