Influence of tip store mass location on wing limit-cycle oscillation

44th AIAA/ASME/ASCE/AHS/ASC Structures, Structural Dynamics, and Materials Conference

Volumn , Issue , 2003, Pages

  Khot, N S ^a   Beran, P S ^a   Zweber, J V ^a   Eastep, F E ^a  

^a AIR FORCE RESEARCH LABORATORY   (United States)

Author keywords

[No Author keywords available]

Indexed keywords

BOUNDARY LAYER FLOW; BOUNDARY LAYERS; COMPUTATION THEORY; STRUCTURAL DYNAMICS; SUPERSONIC AIRCRAFT; VISCOSITY;

AEROELASTIC ANALYSIS; COMPUTATIONAL METHODOLOGY; INTERACTIVE BOUNDARY LAYER; LIMIT CYCLE OSCILLATION (LCO); LIMIT CYCLE OSCILLATIONS; QUENCHING MECHANISMS; TRANSONIC SMALL DISTURBANCES; VISCOSITY INCREASE;

WINGS;

EID: 85086614023     PISSN: None     EISSN: None     Source Type: Conference Proceeding    
DOI: 10.2514/6.2003-1731     Document Type: Conference Paper

References (12)

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11. Beran, P.S., Khot, N.S., Eastep, F.E., Strganac, T.W., and Zweber, J.V., "Effects of Viscosity on Store-Induced Limit-Cycle Oscillation, " 2003 ITEA Aircraft-Stores Compatibility Symposium XIII, Destin FL, February 2003.
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