RISS 학술연구정보서비스

검색
다국어 입력

http://chineseinput.net/에서 pinyin(병음)방식으로 중국어를 변환할 수 있습니다.

변환된 중국어를 복사하여 사용하시면 됩니다.

예시)
  • 中文 을 입력하시려면 zhongwen을 입력하시고 space를누르시면됩니다.
  • 北京 을 입력하시려면 beijing을 입력하시고 space를 누르시면 됩니다.
닫기
    인기검색어 순위 펼치기

    RISS 인기검색어

      KCI등재 SCIE SCOPUS

      Transient performance prediction of an axial compressor considering VIGV operation speeds

      한글로보기

      https://www.riss.kr/link?id=A103788884

      • 0

        상세조회
      • 0

        다운로드
      서지정보 열기
      • 내보내기
      • 내책장담기
      • 공유하기
      • 오류접수

      부가정보

      다국어 초록 (Multilingual Abstract)

      In the present study, transient performance and flow characteristics of a 1.5-stage compressor with VIGV are investigated using CFD.

      The level of accuracy of CFD approach is evaluated by comparing the predicted performance against experimental data of a 3.5-stagecompressor. The main objective of the present research is to quantitatively estimate the performance of transonic axial-flow compressorunder transient operation of VIGV compared to steady-state performances on static IGV condition. The present study is performed toinvestigate the effect of VIGV movement on the performance characteristics when the VIGV setting angle varies with time. The VIGV isset to rotate in the clockwise and counterclockwise directions. The results were compared with steady-state predictions. Reasonable differencesare observed in mass flow rate predictions (2%~6%) between the transient and the steady-state calculations as VIGV operationspeed varies. As VIGV operation speed increases, the difference in mass flow rate also increases. Therefore, a change in work input ofthe compressor is confirmed due to changes in mass flow rate. This is mainly caused by the changes in deviation and incidence anglesdepending on the operation speed and operation direction (clockwise and counterclockwise). The changes in deviation and incidenceangles reflected on the entropy distribution. Even in mid-span, there is variation in angles depending on the operation speed and direction.
      번역하기

      In the present study, transient performance and flow characteristics of a 1.5-stage compressor with VIGV are investigated using CFD. The level of accuracy of CFD approach is evaluated by comparing the predicted performance against experimental data o...

      In the present study, transient performance and flow characteristics of a 1.5-stage compressor with VIGV are investigated using CFD.

      The level of accuracy of CFD approach is evaluated by comparing the predicted performance against experimental data of a 3.5-stagecompressor. The main objective of the present research is to quantitatively estimate the performance of transonic axial-flow compressorunder transient operation of VIGV compared to steady-state performances on static IGV condition. The present study is performed toinvestigate the effect of VIGV movement on the performance characteristics when the VIGV setting angle varies with time. The VIGV isset to rotate in the clockwise and counterclockwise directions. The results were compared with steady-state predictions. Reasonable differencesare observed in mass flow rate predictions (2%~6%) between the transient and the steady-state calculations as VIGV operationspeed varies. As VIGV operation speed increases, the difference in mass flow rate also increases. Therefore, a change in work input ofthe compressor is confirmed due to changes in mass flow rate. This is mainly caused by the changes in deviation and incidence anglesdepending on the operation speed and operation direction (clockwise and counterclockwise). The changes in deviation and incidenceangles reflected on the entropy distribution. Even in mid-span, there is variation in angles depending on the operation speed and direction.

      더보기

      참고문헌 (Reference)

      1 강영석, "다단 천음속 축류형 압축기 성능에 관한 실험적 연구" 한국유체기계학회 14 (14): 96-101, 2011

      2 D. C. Urasek, "Stalled and stallfree performance of axial-flow compressor stage with three inletguide-vane and stator-blade settings" NASA 1977

      3 H. S. Im, "Simulation of 3D multistage axial compressor using a fully conservative sliding boundary condition" 2011

      4 T. W. Song, "Performance prediction of axial flow compressors using stage characteristics and simultaneous calculation of interstage parameters" 215 : 89-98, 2001

      5 J. T. Tomita, "Performance evaluation of a 5kN gas turbine based on specially designed components" 2012

      6 A. Shadaram, "Optimization of variable stator's angle for off design comprresion systems using streamline curvature method" 2009

      7 J. R. Barbosa, "Influence of variable geometry transients on gas turbine performance" 2011

      8 J. R. Barbosa, "Gas turbine transients with controlled variable geometry" 2012

      9 T. C. Park, "Experimental study on detailed flow in a multi-stage transonic axial compressor" 2013 : 332-333, 2013

      10 R. J. Steinke, "Design of 9.271-pressure-ratio five-stage core compressor and overall performance for first three stages" NASA 1986

      1 강영석, "다단 천음속 축류형 압축기 성능에 관한 실험적 연구" 한국유체기계학회 14 (14): 96-101, 2011

      2 D. C. Urasek, "Stalled and stallfree performance of axial-flow compressor stage with three inletguide-vane and stator-blade settings" NASA 1977

      3 H. S. Im, "Simulation of 3D multistage axial compressor using a fully conservative sliding boundary condition" 2011

      4 T. W. Song, "Performance prediction of axial flow compressors using stage characteristics and simultaneous calculation of interstage parameters" 215 : 89-98, 2001

      5 J. T. Tomita, "Performance evaluation of a 5kN gas turbine based on specially designed components" 2012

      6 A. Shadaram, "Optimization of variable stator's angle for off design comprresion systems using streamline curvature method" 2009

      7 J. R. Barbosa, "Influence of variable geometry transients on gas turbine performance" 2011

      8 J. R. Barbosa, "Gas turbine transients with controlled variable geometry" 2012

      9 T. C. Park, "Experimental study on detailed flow in a multi-stage transonic axial compressor" 2013 : 332-333, 2013

      10 R. J. Steinke, "Design of 9.271-pressure-ratio five-stage core compressor and overall performance for first three stages" NASA 1986

      11 L. Gallar, "Compressor variable geometry schedule optimisation using genetic algorithms" 2009

      12 Y. S. Kang, "Aerodynamic design and performance evaluation of multistage highly-loaded axial compressor" 12 (12): 66-71, 2009

      13 "ANSYS Fluent User's Guide"

      14 "ANSYS Fluent UDF manual"

      15 P. R. Spalart, "A one-equation turbulence model for aerodynamics flows" The American Institute of Aeronautics and Astronautics 1992

      더보기

      분석정보

      View

      상세정보조회

      0

      Usage

      원문다운로드

      0

      대출신청

      0

      복사신청

      0

      EDDS신청

      0

      동일 주제 내 활용도 TOP

      더보기

      주제

      연도별 연구동향

      연도별 활용동향

      연관논문

      연구자 네트워크맵

      공동연구자 (7)

      유사연구자 (20) 활용도상위20명

      인용정보 인용지수 설명보기

      학술지 이력

      학술지 이력
      연월일 이력구분 이력상세 등재구분
      2023 평가예정 해외DB학술지평가 신청대상 (해외등재 학술지 평가)
      2020-01-01 평가 등재학술지 유지 (해외등재 학술지 평가) KCI등재
      2012-11-05 학술지명변경 한글명 : 대한기계학회 영문 논문집 -> Journal of Mechanical Science and Technology KCI등재
      2010-01-01 평가 등재학술지 유지 (등재유지) KCI등재
      2008-01-01 평가 등재학술지 유지 (등재유지) KCI등재
      2006-01-19 학술지명변경 한글명 : KSME International Journal -> 대한기계학회 영문 논문집
      외국어명 : KSME International Journal -> Journal of Mechanical Science and Technology
      KCI등재
      2006-01-01 평가 등재학술지 유지 (등재유지) KCI등재
      2004-01-01 평가 등재학술지 유지 (등재유지) KCI등재
      2001-01-01 평가 등재학술지 선정 (등재후보2차) KCI등재
      1998-07-01 평가 등재후보학술지 선정 (신규평가) KCI등재후보
      더보기

      학술지 인용정보

      학술지 인용정보
      기준연도 WOS-KCI 통합IF(2년) KCIF(2년) KCIF(3년)
      2016 1.04 0.51 0.84
      KCIF(4년) KCIF(5년) 중심성지수(3년) 즉시성지수
      0.74 0.66 0.369 0.12
      더보기

      이 자료와 함께 이용한 RISS 자료

      나만을 위한 추천자료

      해외이동버튼