Numerical simulations of a feedback-controlled circular cylinder wake

AIAA Journal

Volumn 44, Issue 6, 2006, Pages 1266-1276

  Siegel, Stefan ^a,b,c   Cohen, Kelly ^a,b,c   McLaughlin, Thomas ^a,c,d  

^a UNITED STATES AIR FORCE ACADEMY   (United States)

^b Department of Aeronautics ^*  (United States)

^c AIAA   (United States)

^d Aeronautics Research Center   (United States)

Author keywords

[No Author keywords available]

Indexed keywords

DIFFERENTIAL FEEDBACK; FEEDBACK FLOW CONTROL; PROPER ORTHOGONAL DECOMPOSITION (POD); THRESHOLD PEAK AMPLITUDE;

COMPUTER SIMULATION; DECOMPOSITION; DRAG; FEEDBACK CONTROL; REYNOLDS NUMBER; VORTEX FLOW;

FLOW CONTROL;

EID: 33746366165     PISSN: 00011452     EISSN: None     Source Type: Journal    
DOI: 10.2514/1.4443     Document Type: Article

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