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Compressible flow involves fluids whose density changes under varying pressure and temperature, primarily applicable to high-velocity gases. Various governing equations, including the continuity, momentum, and energy equations, are essential for analyzing these flows. Key concepts such as stagnation properties, isentropic flow, and choked flow are crucial for understanding flow dynamics in nozzles and diffusers.
References
Module IV_ Compressible Flow.pdfClass Notes
Memorization
What we have learnt
Final Test
Revision Tests
Term: Compressible Flow
Definition: Flow in which the density of a fluid varies significantly with changes in pressure and temperature, typically observed in gases at high velocities.
Term: Stagnation Properties
Definition: Properties that a fluid attains when brought to rest isentropically; includes stagnation temperature, pressure, and enthalpy.
Term: Choked Flow
Definition: A condition in which the flow reaches the speed of sound at the throat of a nozzle, resulting in a maximum mass flow rate irrespective of downstream pressure.
Term: Normal Shocks
Definition: A sudden change in flow properties, characterized by a decrease in Mach number to subsonic, and increases in pressure, temperature, and entropy.