Computational aeroelastics by coupling compressible fluid equations with shell finite-element structure

16th AIAA Applied Aerodynamics Conference

Volumn , Issue , 1998, Pages 41-47

  Onishi, Ryoichi ^a   Kimurat, Toshiya ^a   Guo, Zhihong ^b   Iwamiya, Toshiyuki ^c  

^a JAPAN ATOMIC ENERGY AGENCY   (Japan)

^b INST OF PHYS AND CHEMICAL RESEARCH   (Japan)

^c JAPAN AEROSPACE EXPLORATION AGENCY   (Japan)

Author keywords

[No Author keywords available]

Indexed keywords

AERODYNAMICS; AEROELASTICITY; ASPECT RATIO; FIGHTER AIRCRAFT; STRUCTURAL DYNAMICS;

AUTOMATICALLY GENERATED; COMPRESSIBLE FLUID EQUATIONS; COMPUTATIONAL TOOLS; COUPLING COMPUTATIONS; SHELL FINITE ELEMENTS; SIMULTANEOUS INTEGRATION; STRUCTURAL COUPLING; STRUCTURAL DEFORMATION;

NAVIER STOKES EQUATIONS;

EID: 84983132726     PISSN: None     EISSN: None     Source Type: Conference Proceeding    
DOI: 10.2514/6.1998-2407     Document Type: Conference Paper

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