Aeroelastic prediction of the limit cycle oscillations of a cropped delta wing

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

Volumn 3, Issue , 2005, Pages 1423-1439

  Attar, Peter J ^a,b,c   Gordnier, Raymond E ^a,b,c  

^a AIR FORCE RESEARCH LABORATORY   (United States)

^b Air Vehicles Directorate   (United States)

^c AIAA   (United States)

Author keywords

[No Author keywords available]

Indexed keywords

COMPUTATIONAL METHODS; DELTA WING AIRCRAFT; FINITE ELEMENT METHOD; MATHEMATICAL MODELS; OSCILLATIONS; SHOCK WAVES;

COMPUTATIONAL MODEL; DYNAMIC PRESSURE; GEOMETRIC NONLINEARITIES; LIMIT CYCLE OSCILLATIONS (LCO);

AERODYNAMICS;

EID: 28844473955     PISSN: 02734508     EISSN: None     Source Type: Conference Proceeding    
DOI: 10.2514/6.2005-1915     Document Type: Conference Paper

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