Static and dynamic structural response of an aircraft wing with damage using equivalent plate analysis

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

Volumn , Issue , 2008, Pages

  Krishnamurthy, T ^a,c,d   Tsai, Frank J ^b  

^a NASA LANGLEY RESEARCH CENTER   (United States)

^b Vehicle Analysis Branch   (United States)

^c Durability Damage Tolerance and Reliability Branch   (United States)

^d AIAA ^*

Author keywords

[No Author keywords available]

Indexed keywords

AIRCRAFT WING; ARBITRARY POINTS; EQUIVALENT PLATE ANALYSIS; FLIGHT VEHICLES; OPTIMIZATION APPROACH; OPTIMIZATION PROCEDURES; PLATE GEOMETRIES; PLATE MODELS; SCALE FACTOR; SCALE FACTORS; STATIC AND DYNAMIC; STATIC RESPONSES; STIFFENED PANELS; WIND TUNNEL EXPERIMENTS; WING STRUCTURES;

AIRCRAFT; DYNAMIC RESPONSE; DYNAMICS; ELECTRIC LOAD SHEDDING; EQUIVALENCE CLASSES; FORECASTING; OPTIMIZATION; STATIC ANALYSIS; STIFFNESS; STRUCTURAL DYNAMICS; STRUCTURAL OPTIMIZATION; VEHICLES; WINGS;

PLATES (STRUCTURAL COMPONENTS);

EID: 77957822083     PISSN: 02734508     EISSN: None     Source Type: Conference Proceeding    
DOI: None     Document Type: Conference Paper

References (12)

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