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Effects of centerline curvature and cross-sectional shape transitioning in the subsonic diffuser of the F-5 fighter jet I. H. Ibrahim
The Journal of Mechanical Science and Technology, vol. 22, no. 10, pp.1993-1997, 2008
Abstract : 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.
Keyword :
S-duct; Curved diffuser; Cross-sectional shape; F-5; Distortion; Recovery
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