Engineering, 01.10.2019 19:30 mivantechenko9751
The mach number of an ideal ramjet is 2.88, and the external temperature is 400 ° r. the flow rate of air through the engine is 85 lbm/s. because of thermal limits of the materials, the burner exit total temperature is 3150 "r. the heating value of the fuel is 17,900 btu/ibm. what are the developed thrust, dimensionless thrust, fuel ratio, and tsfc for this engine?
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The mach number of an ideal ramjet is 2.88, and the external temperature is 400 ° r. the flow rate o...
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