Experiments on heave/pitch limit-cycle oscillations of a supercritical airfoil close to the transonic dip

Journal of Fluids and Structures

Volumn 19, Issue 1, 2004, Pages 1-16

  Dietz, G ^a   Schewe, G ^a   Mai, H ^a  

^a GERMAN AEROSPACE CENTER DLR   (Germany)

Author keywords

[No Author keywords available]

Indexed keywords

BOUNDARY LAYERS; COMPUTER SIMULATION; DEGREES OF FREEDOM (MECHANICS); TRANSONIC FLOW; DAMPING; OSCILLATIONS;

FLOW CONDITIONS; TRANSONIC DIP;

AIRFOILS;

AERODYNAMICS; AEROELASTICITY; AEROFOIL; AIRCRAFT; FLOW SEPARATION; FLUTTER; FLUID-STRUCTURE INTERACTION; WIND TUNNEL;

BOUNDARY-LAYER TRANSITION; LIMIT-CYCLE OSCILLATIONS;

EID: 1142281883     PISSN: 08899746     EISSN: None     Source Type: Journal    
DOI: 10.1016/j.jfluidstructs.2003.07.019     Document Type: Article

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