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A pilot flying his ultralight aircraft at a speed of 60 mph. Under standard atmospheric conditions, what would be the maximum pressure on the pilots hand if he extended his hand into the windstream?
consider a steam rankine cycle with superheat. the maximum temperature and pressure are 540 c and 60 bar and the
1.determine the specific volume of superheated nitrogen gas at an absolute pressure of 678 kpa and -134degc based on a
an air-standard brayton cycle is utilized as a jet propulsion engine. the aircraft flies at an altitude of 5000 m at a
Air enters a turbine at 40 kN/m2, 900 C, and leaves at 10 kN/m2. The flow is reversible and adiabatic. Inlet velocity is quite low and outlet velocity is 150 m/s through a cross-sectional area of 0.20 m2. Calculate the power output in kW.
a gas is contained in a vertical piston-cylinder arrangement. the 50-lbm piston initially rests on the bottom stops.
nitrogen n2 initially occupying 0.1 m3 at 6 bar 2478c undergoes an internally reversible expansion during which pv 1.20
Lift coefficient (Cl) and lift (L), An airfoil of surface area 1ft squared is tested for lift (L) in a wind tunnel. At an angle of attack of 5 degrees with standard air of density 0.0024 slugs/ft cube at a speed of 100 ft/sec
refrigerent r-134a at 140 kpa and minus 10 degc is comressed by adiabatic 0.7 kw compressor to an exit state of 700 kpa
Determine the temperature of the electric heater element and drawing of the temperature profile.
find the transfer function for the following impulse responsefind the transfer function for the following impulse
At a section in a passage, the pressure is 150 kPa (abs), the temperature is 10 deg C, and the speed is 120 m/s. For isentropic flow of air, determine the Mach number at the point where the pressure is 50 kPa (abs). Sketch the passage shape.
a thin flat plate is installed in a water tunnel as a splitter. the plate is 0.3 m long and 1 m wide. the freestream
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