Fluid physics and surrogate modeling of a low Reynolds number flapping rigid flat plate

28th AIAA Applied Aerodynamics Conference

Volumn 1, Issue , 2010, Pages

  Trizila, Pat ^a   Kang, Chang Kwon ^a   Aono, Hikaru ^a   Visbal, Miguel ^b   Shyy, Wei ^a,c  

^a UNIVERSITY OF MICHIGAN   (United States)

^b AIR FORCE RESEARCH LABORATORY   (United States)

^c AFRL/RBAC ^*  (United States)

Author keywords

[No Author keywords available]

Indexed keywords

ASPECT RATIO; FIGHTER AIRCRAFT; FLOW CONTROL; KINEMATICS; LIFT; NAVIER STOKES EQUATIONS; REYNOLDS NUMBER; WAKES; WIND TUNNELS;

AERODYNAMIC FORCES; ENVIRONMENTAL SENSITIVITIES; LEADING-EDGE VORTICES; LOW REYNOLDS NUMBER; NAVIER STOKES SOLUTION; POWER PERFORMANCE; POWER REQUIREMENT; QUASI-STEADY MODEL;

VORTEX FLOW;

EID: 78649527731     PISSN: None     EISSN: None     Source Type: Conference Proceeding    
DOI: 10.2514/6.2010-5081     Document Type: Conference Paper

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