Extensive wind tunnel tests measurements of dynamic stall phenomenon for the OA209 airfoil including 3D effects

33rd European Rotorcraft Forum 2007, ERF33

Volumn 1, Issue , 2007, Pages 320-335

  Le Pape, Arnaud ^a   Pailhas, Guy ^a   David, Frédéric ^a   Deluc, Jean Michel ^a  

^a ONERA   (France)

Author keywords

Dynamic stall; LDV; OA209 airfoil; PIV; Wind tunnel tests

Indexed keywords

3D EFFECTS; AERODYNAMIC FORCES; DYNAMIC STALL; DYNAMIC STALLS; FLOW FIELD MEASUREMENT; LASER DOPPLER VELOCIMETRY; MEASUREMENT TECHNIQUES; PARTICLE IMAGE VELOCIMETRY TECHNIQUE; REYNOLDS; SPAN WINGS; TIP VORTEX; UNSTEADY PRESSURE DISTRIBUTION; WIND TUNNEL TESTS;

AERODYNAMIC CONFIGURATIONS; AIRCRAFT; AIRFOILS; DOPPLER EFFECT; FLOW FIELDS; FLOW VISUALIZATION; FRICTION; HELICOPTER ROTORS; LASER DOPPLER VELOCIMETERS; STATISTICAL TESTS; VELOCITY MEASUREMENT; WIND STRESS; WIND TUNNELS;

THREE DIMENSIONAL;

EID: 77954221141     PISSN: None     EISSN: None     Source Type: Conference Proceeding    
DOI: None     Document Type: Conference Paper

References (17)

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