본문 바로 가기

로고

국내 최대 기계 및 로봇 연구정보
통합검색 화살표
  • STAR-CCM+®
  • 기술보고서

    기술보고서 게시판 내용
    타이틀 Transition Mixing Study Empirical Model Report
    저자 R. Srinivasan and C. White
    Keyword Combustor; Transition-mixing; Computer-model; Empirical-model
    URL http://gltrs.grc.nasa.gov/reports/1988/CR-182139.pdf
    보고서번호 NASA CR-182139
    발행년도 1988
    출처 NASA Glenn Research Center
    ABSTRACT The empirical model developed in the NASA Dilution Jet Mixing Program has been extended to include the curvature effects of transition liners. This extension is based on the results of 3-D numerical model results generated under this contract. The empirical model results agree well with the numerical model results for all the test casesevaluated. The empirical model shows faster mixing rates compared to the numerical model. Both models show drift of jets toward the inner wall of a turning duct. The structure of the jets from the inner wall does not exhibit the familiar kidney-shaped structures observed for the outer wall jets or for jets injected in rectangular ducts.

    서브 사이드

    서브 우측상단1