2022
DOI: 10.1016/j.oceaneng.2022.112120
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Vortical flow characteristics of a slender delta wing in ground effect

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Cited by 8 publications
(3 citation statements)
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“…Furthermore, while the Q-criterion, λ 2 -criterion, and ∆-criterion are effective in binary classification, categorizing regions as vortical or non-vortical, they do not inherently provide direct quantification of vortex strength or intensity [28]. Evaluating vortex strength is often crucial for in-depth analysis of vortex dynamics, comparative studies between vortices, and various related objectives [29,30]. Researchers typically need to perform supplementary analyses to calculate circulation, maximum vorticity, core radius, or other relevant parameters to obtain strength information [29,30].…”
Section: Introductionmentioning
confidence: 99%
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“…Furthermore, while the Q-criterion, λ 2 -criterion, and ∆-criterion are effective in binary classification, categorizing regions as vortical or non-vortical, they do not inherently provide direct quantification of vortex strength or intensity [28]. Evaluating vortex strength is often crucial for in-depth analysis of vortex dynamics, comparative studies between vortices, and various related objectives [29,30]. Researchers typically need to perform supplementary analyses to calculate circulation, maximum vorticity, core radius, or other relevant parameters to obtain strength information [29,30].…”
Section: Introductionmentioning
confidence: 99%
“…Evaluating vortex strength is often crucial for in-depth analysis of vortex dynamics, comparative studies between vortices, and various related objectives [29,30]. Researchers typically need to perform supplementary analyses to calculate circulation, maximum vorticity, core radius, or other relevant parameters to obtain strength information [29,30].…”
Section: Introductionmentioning
confidence: 99%
“…In addition, the slender body was the basic geometry of fighter aircraft and missiles, hence, the highly random asymmetric flow was coupled with wings and induces a yawing moment [ 3 ], which was even largely great beyond the control by the rudder of a missile [ 2 , 4 , 5 ]. In addition, the development and bursting of asymmetric vortices were sensitive to the structure of the wings and the coupling position at high AoA [ 6 , [7] , [8] ]. During side-force and yawing, the controllability of the aircraft and missile was reduced, thereby resulting in a failed mission because the desired tracks of the fighter aircraft and missiles were changed.…”
Section: Introductionmentioning
confidence: 99%