Aeroelastic airfoil with free play at angle of attack with gust excitation

AIAA Journal

Volumn 48, Issue 2, 2010, Pages 427-442

  Tang, Deman ^a   Dowell, Earl H ^a  

^a Duke University   (United States)

Author keywords

[No Author keywords available]

Indexed keywords

AEROELASTIC RESPONSE; AIRFOIL SECTION; AIRLOADS; ANALYTICAL APPROACH; CONTROL SURFACES; DUKE UNIVERSITY; EXPERIMENTAL INVESTIGATIONS; FINITE STATE; GUST EXCITATION; GUST GENERATORS; GUST RESPONSE; LIMIT CYCLE OSCILLATIONS; PITCH ANGLE; PITCH RESPONSE; QUANTITATIVE AGREEMENT; REASONABLE ACCURACY; SELF - EXCITED; SLOTTED CYLINDERS; THEORETICAL APPROACH;

ANGLE OF ATTACK; COMPUTATIONAL EFFICIENCY; FIGHTER AIRCRAFT; WIND TUNNELS;

AIRFOILS;

EID: 76949096758     PISSN: 00011452     EISSN: None     Source Type: Journal    
DOI: 10.2514/1.44538     Document Type: Conference Paper

References (16)

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