Influence of finite span and sweep on active flow control efficacy

Collection of Technical Papers - AIAA Applied Aerodynamics Conference

Volumn 2, Issue , 2007, Pages 1230-1253

  Greenblatt, David ^a   Washburn, Anthony E ^b,c  

^a TECHNISCHE UNIVERSITÄT BERLIN   (Germany)

^b NASA LANGLEY RESEARCH CENTER   (United States)

^c Flow Physics and Control Branch   (United States)

Author keywords

[No Author keywords available]

Indexed keywords

ANGLE OF ATTACK; MATHEMATICAL MODELS; MOMENTUM; PERTURBATION TECHNIQUES; WINGS;

ACTIVE FLOW CONTROL; FINITE SPAN; LEADING-EDGE PERTURBATIONS; ZERO MASS-FLUX;

FLOW CONTROL;

EID: 35649001935     PISSN: 10485953     EISSN: None     Source Type: Conference Proceeding    
DOI: 10.2514/6.2007-4275     Document Type: Conference Paper

References (16)

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