Measurements of the flow due to a rapidly pitching plate using time resolved high resolution PIV

Aerospace Science and Technology

Volumn 44, Issue , 2015, Pages 4-17

  Buchner, A J ^a,c   Soria, J ^a,b  

^a MONASH UNIVERSITY   (Australia)

^b KING ABDULAZIZ UNIVERSITY   (Saudi Arabia)

^c Princeton University   (United States)

Author keywords

Dynamic stall; Massively separated flow; Particle image velocimetry (PIV); Pitching airfoil; Vortex tracking

Indexed keywords

AIRFOILS; FLOW VISUALIZATION; HELICOPTER ROTORS; MICRO AIR VEHICLE (MAV); REYNOLDS EQUATION; REYNOLDS NUMBER; TOPOLOGY; UNMANNED VEHICLES; VELOCIMETERS; VELOCITY MEASUREMENT; WAKES; WIND TURBINES;

DYNAMIC STALLS; MASSIVELY SEPARATED FLOW; PARTICLE IMAGE VELOCIMETRIES; PITCHING AIRFOILS; VORTEX TRACKING;

PLATES (STRUCTURAL COMPONENTS);

EID: 84942078187     PISSN: 12709638     EISSN: None     Source Type: Journal    
DOI: 10.1016/j.ast.2014.04.007     Document Type: Article

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