Experimental study of two AIRBUS/ONERA airfoils in near stall conditions. Part I: Boundary layers

Aerospace Science and Technology

Volumn 7, Issue 6, 2003, Pages 439-449

  Gleyzes, Christian ^a   Capbern, Patrick ^b  

^a ONERA   (France)

^b AIRBUS   (France)

Author keywords

Bidimensional flows; Boundary layers; Database; Experiments; Laser velocimetry; Stall

Indexed keywords

BOUNDARY LAYER FLOW; CALIBRATION; COMPUTATIONAL FLUID DYNAMICS; DATABASE SYSTEMS; LASER DOPPLER VELOCIMETERS; LIFT; PRESSURE DISTRIBUTION; REYNOLDS NUMBER; STALL INDICATORS; WAKES;

BIDIMENSIONAL FLOWS; MACH NUMBER;

AIRFOILS;

EID: 0347354891     PISSN: 12709638     EISSN: None     Source Type: Journal    
DOI: 10.1016/S1270-9638(03)00045-2     Document Type: Article

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