A stochastic approach for predicting bifurcation of a pitch and plunge airfoil

21st AIAA Applied Aerodynamics Conference

Volumn , Issue , 2003, Pages

  Millman, D R ^a   King, I P ^a   Beran, P S ^b  

^a AIR FORCE INSTITUTE OF TECHNOLOGY   (United States)

^b AIR FORCE RESEARCH LABORATORY   (United States)

Author keywords

[No Author keywords available]

Indexed keywords

AERODYNAMICS; AEROELASTICITY; AIRFOILS; DISTRIBUTION FUNCTIONS; EQUATIONS OF MOTION; INTELLIGENT SYSTEMS; PROBABILITY DISTRIBUTIONS; STOCHASTIC SYSTEMS; UNCERTAINTY ANALYSIS;

AEROELASTIC SYSTEM; INPUT UNCERTAINTY; ORTHOGONAL POLYNOMIAL; POLYNOMIAL CHAOS EXPANSION; SPECTRAL STOCHASTIC METHODS; STOCHASTIC APPROACH; SUBCRITICAL RESPONSE; TIME INTEGRATION;

MONTE CARLO METHODS;

EID: 85067318064     PISSN: None     EISSN: None     Source Type: Conference Proceeding    
DOI: 10.2514/6.2003-3515     Document Type: Conference Paper

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