An analytical method in computational aeroelasticity based on Wagner function

ICAS-Secretariat - 25th Congress of the International Council of the Aeronautical Sciences 2006

Volumn 3, Issue , 2006, Pages 1808-1814

  Shams, Sh ^a   Haddadpour, H ^b   Sadr Lahidjani, M H ^a   Kheiri, M ^b  

^a AMIRKABIR UNIVERSITY OF TECHNOLOGY   (Iran)

^b SHARIF UNIVERSITY OF TECHNOLOGY   (Iran)

Author keywords

Aeroelasticity; Flutter; Integro differential system of equations; Sharp edged gust

Indexed keywords

AIRFOILS; DEGREES OF FREEDOM (MECHANICS); EQUATIONS OF MOTION; FLUTTER (AERODYNAMICS); INTEGRAL EQUATIONS; ORDINARY DIFFERENTIAL EQUATIONS;

ANALYTICAL METHOD; COMPUTATIONAL AERO ELASTICITY; FLUTTER; INTEGRAL FUNCTION; INTEGRO-DIFFERENTIAL SYSTEM; INTEGRO-DIFFERENTIAL SYSTEM OF EQUATION; SHARP-EDGED GUST; SYSTEMS OF EQUATIONS; TWO-DEGREE-OF-FREEDOM; WAGNER'S FUNCTION;

AEROELASTICITY;

EID: 84896919286     PISSN: None     EISSN: None     Source Type: Conference Proceeding    
DOI: None     Document Type: Conference Paper

References (18)

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