Aerospace Propulsion and Orbital Mechanics Fundamentals
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Engine Performance Parameters
Where: $m_{\dot{a}}$ = air mass flow, $m_{\dot{f}}$ = fuel mass flow, $V_{EG}$ = exhaust gas velocity, $V_{Air}$ = aircraft speed, $P_e$ = exhaust pressure, $P_0$ = ambient pressure, $A_e$ = nozzle exit area.
Propulsive Power
Propulsive Power: (Thrust times aircraft velocity). Note: zero at start of takeoff.
Fuel consumed per unit thrust.
Efficiency Metrics
Thermal Efficiency: Ratio of output power to input heat energy.
Propulsive Efficiency: Depends on the ratio of aircraft speed to exhaust jet speed.
Engine Components and Cycles
Subsonic Diffuser: Reduces air velocity, recovers pressure before the compressor.
Supersonic Diffuser: Slows supersonic flow to subsonic using shock waves.
Compressors:
- Radial (Centrifugal): High