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In early development of gas turbine engines, the pressure ratio was low, the isentropic efficiency of components was low, and metallurgy limited upper operating temperature of gases entering the turbine. Consider standard inlet conditions of 1.0 atm, 25 C, a pressure ratio of 4 across compressor, and an upper operating temperature limit of 600 C, what is the minimum isentropic efficiency of compressor and turbine (assume equal for simplicity), for which the engine will just begin to produce net power output, i.e., break-even?
a system consists of nitrogen n2 in a piston-cylinder assembly initially at p1 20 lbfin2 and occupying a volume of
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a normal shock wave exists in mach 2 stream of air having temperature and pressure of 45degf and 30 psia respectively.
Evaluate the maximum height reached by the sphere, and the distance traveled by the block.
a brinell hardness measurement is made on a nickel alloy using a 0.01 m diameter sphere of tungsten carbide. a load of
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Find Stall Speed (KEAS) at 1 G, 0 deg AOB and find Stall Speed (KEAS), level flight 70 deg AOB (2.9 G)
Calculate the value of forces P and Q for each test using the method of sections technique.
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a stack was sampled for 8 minutes. the gas velocity at stack conditions through the sampler was 15.0 ms and the area
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