International Journal of Fluid Machinery and Systems

한국유체기계학회 (Korean Society for Fluid machinery)
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Development of a Simulation Method of Surge Transient Flow Phenomena in a Multistage Axial Flow Compressor and Duct System

  • 투고 : 2013.05.31
  • 심사 : 2013.09.27
  • 발행 : 2013.12.30
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초록

A practical method of surge simulation in a system of a high-pressure-ratio multistage axial flow compressor and ducts, named SRGTRAN, is described about the principal procedures and the details. The code is constructed on the basis of one-dimensional stage-by-stage modeling and application of fundamental equations of mass, momentum, and energy. An example of analytical result on surge behaviors is included as an experimental verification. It will enable to examine the transient flow phenomena caused by possible compressor surges and their influences on the system components in plant systems including high-pressure-ratio axial compressors or gas turbines.

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참고문헌

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피인용 문헌

  1. Surge Phenomena Analytically Predicted in a Multi-stage Axial Flow Compressor System in the Reduced-Speed Zone vol.7, pp.3, 2014, https://doi.org/10.5293/IJFMS.2014.7.3.110
  2. A Study on the Fundamental Surge Frequencies in Multi-Stage Axial Flow Compressor Systems vol.7, pp.4, 2014, https://doi.org/10.5293/IJFMS.2014.7.4.160
  3. Analytical Surge Behaviors in Systems of a Single-stage Axial Flow Compressor and Flow-paths vol.9, pp.1, 2016, https://doi.org/10.5293/IJFMS.2016.9.1.001