Vortex flows over 50° sweep delta wing at low Reynolds number

Kongqi Donglixue Xuebao/Acta Aerodynamica Sinica

Volumn 28, Issue 2, 2010, Pages 174-179

  Chen, Lan ^a,b   Wang, Jin Jun ^a   Zuo, Lin Xian ^a   Feng, Li Hao ^a  

^a PEKING UNIVERSITY   (China)

^b CHINA AERODYNAMICS RESEARCH AND DEVELOPMENT CENTER   (China)

Author keywords

Low Reynolds number; Non slender delta wing; Vortex flows

Indexed keywords

ATTACHMENT LINES; COMPUTATIONAL SIMULATION; COMPUTATIONAL STUDIES; DELTA WING VORTICES; DELTA WINGS; EXPERIMENTAL INVESTIGATIONS; LEADING EDGE; LEADING-EDGE VORTICES; LOW REYNOLDS NUMBER; PRIMARY VORTEX; UPPER SURFACE; VORTEX STRUCTURES;

ANGLE OF ATTACK; REYNOLDS NUMBER; VORTEX FLOW;

DELTA WING AIRCRAFT;

EID: 77952788472     PISSN: 02581825     EISSN: None     Source Type: Journal    
DOI: None     Document Type: Article

References (10)

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