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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.
the laminar flame speed of a premixed stoichiometric mixture of propane?air at 1 atm and 298 k is 0.4 ms. estimate the
compare it with efficiency of an otto cycle operating with the same maximum pressure?
1 nitrogen gas flows into a convergent nozzle at a pressure of 225kpa a temperature of 440k and with a very low inlet
problem 1a plane stress element is subjected to stress componentssigmax 50 mpa sigmay -10 mpa and tauxy 40 mpa.1
Compare the time and cost of using the following three alternative methods for casting the concrete for the wall: 1) direct chute 2) pumped 3) crane and bucket.
the angular velocity of linkabis wab 4.6 rads.determine the magnitude of the velocity of the block at cat the instant
Use thin airfoil theory to show that the pressure coefficient across the length of the ellipse in the stream-wise direction is constant when it is assumed T
Draw the shear force diagram for the beam and determine the position and magnitude of the maximum bending moment.
water flowing in a horizontal 30 cm diameter pipe at 5 ms and 300 kpa gage enters a 90o bend reducing section which
a closed tank has an enclosed airspace above the surface of water which fills the tank to a depth of something over a
liquid water at 50degc and 1 mpa is mixed with superheated steam at 200degc and 1 mpa in an open feedwater heater
a closed rigid container has a volume of 85 liters. the system contains steam at 2 bar and has a quality of 0.9.
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