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Wan et al., 2011 - Google Patents

Investigation of air tab's effect in supersonic jets

Wan et al., 2011

Document ID
7979894004206224224
Author
Wan C
Yu S
Publication year
Publication venue
Journal of Propulsion and Power

External Links

Snippet

MIXING enhancement in supersonic jet flow has been investigated extensively in the past two decades due to its relevance in reducing the jet noise in high-speed civil transport (HSCT) aircraft and suppressing the infrared signature of the jet engine exhausts. The solid …
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