• Title/Summary/Keyword: 원심/사류압축기

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Aerodynamic Design Program for Centrifugal/Mixed-flow Compressors - Part I : Meanline Design and Performance Prediction - (원심/사류압축기의 공력설계 프로그램 개발 - 제1부 : 평균유선 설계/성능해석 -)

  • Oh, Jong-Sik
    • 유체기계공업학회:학술대회논문집
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    • 2003.12a
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    • pp.457-463
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    • 2003
  • A general program of meanline design and/or performance prediction for centrifugal/mixed-flow compressors is successfully commercialized using various empirical loss models. 4 types of diffusers, 3 types of exit elements, shrouded/unshrouded impellers and real gas option are included in the program capabilities. Total 16 cases of benchmark test results proved its reliability to be effectively utilized in the development processes.

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Aerodynamic Design Program for Centrifugal/Mixed-flow Compressors - Part II : Three Dimensional Profile Design of Impellers - (원심/사류압축기의 공력설계 프로그램 개발 - 제2부 : 임펠러의 3차원 형상설계 -)

  • Oh, Jong-Sik
    • 유체기계공업학회:학술대회논문집
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    • 2003.12a
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    • pp.464-468
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    • 2003
  • A general program of three dimensional profile design of impellers for centrifugal/fixed-flow compressors is successfully commercialized using Bezier curves and quasi-3D flow analysis methods. Control points for meridional hub and shroud contours and blade camberline angles are arbitrarily changed to give smooth Bezier curves. With specified blade normal thicknesses, contructed geometry is instantly analyzed using flow analysis methods to be checked.

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A study on Windmilling Start Performance of Micro Turbo-jet Engine (초소형 엔진의 윈드밀링 시동 성능 해석)

  • Kim, Wan-Jo;Park, Hwi-Seob;Roh, Tae-Seong
    • Proceedings of the Korean Society of Propulsion Engineers Conference
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    • 2007.11a
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    • pp.319-322
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    • 2007
  • A numerical method for prediction of the Windmilling start performance of micro-turbojet engine has been developed. The method incorporates the available loss correlations and analyses for the estimation of the performance of the major engine components. It has been applied to the micro turbojet engine with the mixed type compressor. The starting performance characteristics on the on/off-design regions have been analysed. Additionally, the sensitivity of each design parameter which has an effect on Windmilling start performance has been analysed.

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A Study on Windmilling Start Performance of Micro Turbo-jet Engine (초소형 엔진의 윈드밀링 시동 성능 해석)

  • Kim, Wan-Jo;Park, Hwi-Seob;Roh, Tae-Seong;Choi, Dong-Whan
    • Journal of the Korean Society of Propulsion Engineers
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    • v.12 no.2
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    • pp.15-23
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    • 2008
  • A numerical method based on the prediction of total pressure loss of major components of the engine has been developed for prediction of the windmilling start performance of micro-turbojet engine. The start performance in on/off design region has been analysed by applying this method to predict windmilling start-able regions of the centrifugal-type engine. The results of this analysis have been validated by comparing with the test data. The effect of each design parameters on windmilling start performance has been analysed for the enlargement of start-able regions.