The flow visualization CFD studies of the fuselage and rolled-up vortex effects of the chengdu J-10-like fighter canard
T Rochmat, S Wibowo, S Iswahyudi… - Modern Applied …, 2018 - ideas.repec.org
Fighter aircrafts with high maneuverability and swiftness are due to fuselage effects, caused
by canard-fuselage-main wing configuration. Even though the flows around fighters are
highly complex, mostly they create rolled-up vortices capable to delay stalls and increase
maximum lifts (Calderon, Wang & Gursul, 2012; Mitchell & Delery, 2001; Boelens, 2012;
Chen, Liu, Guo & Qu, 2015). The vortex dynamics analysis method employment is
introduced, in this case we focus only on the fighter canard. It characterizes the vortex core …
by canard-fuselage-main wing configuration. Even though the flows around fighters are
highly complex, mostly they create rolled-up vortices capable to delay stalls and increase
maximum lifts (Calderon, Wang & Gursul, 2012; Mitchell & Delery, 2001; Boelens, 2012;
Chen, Liu, Guo & Qu, 2015). The vortex dynamics analysis method employment is
introduced, in this case we focus only on the fighter canard. It characterizes the vortex core …
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