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서지반출
Effects of centerline curvature and cross-sectional shape transitioning in the subsonic diffuser of the F-5 fighter jet
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  • Effects of centerline curvature and cross-sectional shape transitioning in the subsonic diffuser of the F-5 fighter jet
  • Effects of centerline curvature and cross-sectional shape transitioning in the subsonic diffuser of the F-5 fighter jet
저자명
Ibrahim. I.H.,Ng. E.Y.K.,Wong. K.,Gunasekaran. R.
간행물명
Journal of mechanical science and technology
권/호정보
2008년|22권 10호|pp.1993-1997 (5 pages)
발행정보
대한기계학회
파일정보
정기간행물|ENG|
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기타
이 논문은 한국과학기술정보연구원과 논문 연계를 통해 무료로 제공되는 원문입니다.
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기타언어초록

Intake geometries result in unwanted secondary flows and formations of vortices which affect the engine performance. This paper investigates the effects of the curvature and cross-sectional shape transitioning of the actual F-5 duct. Two additional different geometries were set up to isolate each parameter; a circular cross-sectional duct with similar centerline configuration and a straight duct with similar cross-sectional transitioning as the F-5 duct. To measure the efficiency of duct flow, the distortion index (DC(60)) and pressure recovery are used. It is found that the straight duct with similar cross-sectional transitioning as the F-5 intake resulted in a 2.1% increase in pressure recovery and an 86% decrease in distortion when compared with the baseline intake. Also, the baseline intake resulted in a 0.5% increase in pressure recovery and a 15% decrease in distortion compared to the constant circular cross-sectional duct.