Effect of wing planform on leading-edge vortex structures

DOI10.1007/S11434-009-0643-ZzbMath1196.76013OpenAlexW1997084948MaRDI QIDQ708028

Jianqiang Tu, Jin-Jun Wang

Publication date: 8 October 2010

Published in: Chinese Science Bulletin (Search for Journal in Brave)

Full work available at URL: https://doi.org/10.1007/s11434-009-0643-z

zbMATH Keywords

low Reynolds number flowlow aspect ratio wingleading-edge vortexsweep angle

Mathematics Subject Classification ID

Experimental work for problems pertaining to fluid mechanics (76-05) Turbulence (76F99)

Cites Work

• Numerical simulations of leading-edge vortex core axial velocity for flow over delta wings

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