Wing-rock limit cycle oscillation prediction based on computational fluid dynamics

Journal of Aircraft

Volumn 45, Issue 3, 2008, Pages 954-961

  Badcock, K J ^a,d,e   Woodgate, M A ^a,d   Allan, M R ^b,d   Beran, P S ^c,f  

^a UNIVERSITY OF LIVERPOOL   (United Kingdom)

^b UNIVERSITY OF GLASGOW   (United Kingdom)

^c AIR FORCE RESEARCH LABORATORY   (United States)

^d Department of Engineering ^*

^e AIAA ^*

^f Multidisciplinary Technologies Center

Author keywords

[No Author keywords available]

Indexed keywords

COMPUTATIONAL FLUID DYNAMICS; EIGENVALUES AND EIGENFUNCTIONS; FLIGHT DYNAMICS; FORECASTING; INVERSE PROBLEMS; LINEAR SYSTEMS; TIME DOMAIN ANALYSIS; WINGS;

COMPUTATIONAL COSTS; COMPUTATIONAL TASK; CRITICAL EIGENVALUES; DYNAMICS INSTABILITIES; INVERSE POWER METHOD; LIMIT CYCLE OSCILLATION (LCO); REDUCED ORDER MODELS; SPARSE LINEAR SYSTEMS;

DELTA WING AIRCRAFT;

EID: 46449116066     PISSN: 00218669     EISSN: 15333868     Source Type: Journal    
DOI: 10.2514/1.32812     Document Type: Article

References (13)

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