A surrogate based approach to reduced-order dynamic stall modeling

Collection of Technical Papers - AIAA/ASME/ASCE/AHS/ASC Structures, Structural Dynamics and Materials Conference

Volumn , Issue , 2010, Pages

  Glaz, Bryan ^a   Liu, Li ^a   Friedmann, Peretz P ^a   Bain, Jeremy ^b   Sankar, Lakshmi N ^b  

^a UNIVERSITY OF MICHIGAN   (United States)

^b Georgia Institute of Technology   (United States)

Author keywords

[No Author keywords available]

Indexed keywords

AEROELASTICITY; ANGLE OF ATTACK; COMPUTATIONAL FLUID DYNAMICS; STRUCTURAL DYNAMICS; TURBOMACHINE BLADES;

AERODYNAMIC RESPONSE; COMPUTATIONAL EXPENSE; DESIGN OPTIMIZATION; FREESTREAM MACH NUMBER; HELICOPTER ROTOR BLADES; NONLINEAR UNSTEADY AERODYNAMIC MODELS; REDUCED ORDER MODELS; SHOCK INDUCED SEPARATION;

AERODYNAMIC STALLING;

EID: 84855628500     PISSN: 02734508     EISSN: None     Source Type: Conference Proceeding    
DOI: 10.2514/6.2010-3042     Document Type: Conference Paper

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