Engineering, 17.04.2020 18:17 Izayoi
An ideal turbojet ingests 192 lbm/s of air at an altitude of 22000ft it flies at a mach number of 0.88 and the compressure pressure ratio is 17 the fuel has a heating value of 17900 and the burner exit total temperature is 2350 find the developed thrust dimensionless thrust and TSFC..
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The higher the astm grain-size number, the coarser the grain is. a)-true b)-false
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Engineering, 04.07.2019 18:10
What are the two (02) benefits, which may result from a successful implementation of preventive maintenance (pm) program in an organization? (clo3)a)- lean manufacturing b)-overlapping responsibilities c)-the planner is not qualified d)-accurate contractor information e)-reduction in equipment redundancies f)-accurate stores information
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Engineering, 04.07.2019 19:10
Apressure vessel with an r/t 20 cannot be treated as thin walled vessel. a)-trune b)- false
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An ideal turbojet ingests 192 lbm/s of air at an altitude of 22000ft it flies at a mach number of 0....
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