Engineering, 22.08.2019 05:30 cravingnafi202
Air enters the compressor of a gas turbine at 70°f and 0.8 psig and leaves the compressor at 300°f and 36 psig. it leaves the nozzle of the gas turbine at 650°f and 2.5 psig. with the atmospheric pressure of 14.7psi and nozzle exit area of 4 in^2: determine the following: a) pressure ratio b) ideal efficiency c) thrust generated by the engine in lbf d) mach number
Answers: 3
Engineering, 04.07.2019 18:10
Give heat transfer applications for the following, (i) gas turbines (propulsion) ) gas turbines (power generation). (iii) steam turbines. (iv) combined heat and power (chp). (v) automotive engines
Answers: 1
Engineering, 04.07.2019 18:10
The filament of an incandescent lamp has a temperature of 2000k. calculate the fraction of radiation emitted in the visible light band if the filament is approximated as blackbody
Answers: 2
Engineering, 04.07.2019 18:20
Steam enters a converging nozzle at 3.0 mpa and 500°c with a at 1.8 mpa. for a nozzle exit area of 32 cm2, determine the exit velocity, mass flow rate, and exit mach number if the nozzle: negligible velocity, and it exits (a) is isentropic (b) has an efficiency of 94 percent
Answers: 2
Engineering, 04.07.2019 18:20
Atank with constant volume contains 2.27 kg of a mixture of water phases (liquid-vapor). in the initial state the temperature and the quality are 127 °c and 0.6, respectively. the mixture is heated until the temperature of 160 oc is reached. illustrate the process in a t-v diagram. then, determine (1) the mass of the vapor in kg at the initial state, (2) the final pressure in kpa.
Answers: 3
Air enters the compressor of a gas turbine at 70°f and 0.8 psig and leaves the compressor at 300°f a...
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