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Keywords: Core length
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Journal Articles
Supersonic jet flow control using semi-circular corrugated tabs
Available to Purchase
Aircraft Engineering and Aerospace Technology: An International Journal (2019) 91 (10): 1340–1352.
Published: 19 August 2019
... is strongly due to the small-scale vortices shed from the tabs and the mixed effect of the corrugation locations and expansion ratio. The maximum percentage reduction in core length is about 73.6 per cent for the jet with semi-circular corrugated Tab A at NPR 5, whereas it is 71.4 and 67.1 per cent for Tabs B...
