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  2. Choked flow - Wikipedia

    en.wikipedia.org/wiki/Choked_flow

    For homogeneous fluids, the physical point at which the choking occurs for adiabatic conditions is when the exit plane velocity is at sonic conditions; i.e., at a Mach number of 1. [1] [2] [3] At choked flow, the mass flow rate can be increased only by increasing the upstream density of the substance.

  3. Compressor characteristic - Wikipedia

    en.wikipedia.org/wiki/Compressor_characteristic

    Choking is the condition which occurs in the compressor in which it operates at very high mass flow rate and flow through the compressor can't be further increased as mach number at some part of the compressor reach to unity i.e. to sonic velocity and the flow is said to be choked. In compressor maximum volume flow rate is limited by cross ...

  4. Compressor map - Wikipedia

    en.wikipedia.org/wiki/Compressor_map

    A compressor map is a chart which shows the performance of a turbomachinery compressor. This type of compressor is used in gas turbine engines, for supercharging reciprocating engines and for industrial processes, where it is known as a dynamic compressor. A map is created from compressor rig test results or predicted by a special computer program.

  5. Researchers outline how to save yourself from choking if you ...

    www.aol.com/lifestyle/2016-08-01-how-to-save...

    The thought of choking, especially when there's no one there to help, is terrifying. Unfortunately, that fear is not unfounded: choking is the cause of thousands of deaths per year. A new article ...

  6. Fanno flow - Wikipedia

    en.wikipedia.org/wiki/Fanno_flow

    Differential equations can also be developed and solved to describe Fanno flow property ratios with respect to the values at the choking location. The ratios for the pressure, density, temperature, velocity and stagnation pressure are shown below, respectively. They are represented graphically along with the Fanno parameter.

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  8. Surge in compressors - Wikipedia

    en.wikipedia.org/wiki/Surge_in_compressors

    Compressor surge is a form of aerodynamic instability in axial compressors or centrifugal compressors.The term describes violent air flow oscillating in the axial direction of a compressor, which indicates the axial component of fluid velocity varies periodically and may even become negative.

  9. Compressor stall - Wikipedia

    en.wikipedia.org/wiki/Compressor_stall

    Axi-symmetric stall, more commonly known as compressor surge; or pressure surge, is a complete breakdown in compression resulting in a reversal of flow and the violent expulsion of previously compressed air out through the engine intake, due to the compressor's inability to continue working against the already-compressed air behind it.

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