A turbojet engine is powering a fighter airplane. It has the following characteristics: Flight Mach number 0.8 Altitude 65,000 ft Ambient temperature 216.7 K Ambient pressure 5.5 kPa Fuel heating value 42,700 kJ/kg Thrust force 53.4 kN 45 kg/s 2.5 kg/s Air mass flow rate Fuel mass flow rate Aircraft gross weight (65,000 ft) 156 kN Calculate: 1. The specific thrust, 2. TSFC, 3. The exit velocity, 4. The thermal efficiency, 5. The propulsive efficiency, 6. The overall efficiency
Energy transfer
The flow of energy from one region to another region is referred to as energy transfer. Since energy is quantitative; it must be transferred to a body or a material to work or to heat the system.
Molar Specific Heat
Heat capacity is the amount of heat energy absorbed or released by a chemical substance per the change in temperature of that substance. The change in heat is also called enthalpy. The SI unit of heat capacity is Joules per Kelvin, which is (J K-1)
Thermal Properties of Matter
Thermal energy is described as one of the form of heat energy which flows from one body of higher temperature to the other with the lower temperature when these two bodies are placed in contact to each other. Heat is described as the form of energy which is transferred between the two systems or in between the systems and their surrounding by the virtue of difference in temperature. Calorimetry is that branch of science which helps in measuring the changes which are taking place in the heat energy of a given body.
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