Dynamic stall alleviation using a deformable leading edge concept - A numerical study

Journal of Aircraft

Volumn 40, Issue 1, 2003, Pages 77-85

  Sahin, Mehmet ^a   Sankar, Lakshmi N ^a   Chandrasekhara, M S ^b   Tung, Chee ^c  

^a GEORGIA INSTITUTE OF TECHNOLOGY   (United States)

^b NAVAL POSTGRADUATE SCHOOL   (United States)

^c NASA AMES RESEARCH CENTER   (United States)

Author keywords

[No Author keywords available]

Indexed keywords

AIRCRAFT; AIRFOILS; DEFORMATION; DRAG; HYSTERESIS; STRENGTH OF MATERIALS;

PITCHING MOMENTS;

STALL INDICATORS;

EID: 0037226231     PISSN: 00218669     EISSN: 15333868     Source Type: Journal    
DOI: 10.2514/2.3060     Document Type: Article

References (12)

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