Equivalent plate analysis of aircraft wing with discrete source damage

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

Volumn 10, Issue , 2006, Pages 7445-7460

  Krishnamurthy, T ^a,b,c   Mason, Brian H ^a,b,c  

^a NASA LANGLEY RESEARCH CENTER   (United States)

^b Computational Structures and Materials Branch ^*  (United States)

^c AIAA   (United States)

Author keywords

[No Author keywords available]

Indexed keywords

EQUIVALENT PLATES; LUMPED MASS MATRIX; MASS DISTRIBUTION; PROPORTIONALITY CONSTANT;

COMPUTATIONAL METHODS; FLIGHT DYNAMICS; MATHEMATICAL MODELS; PLATES (STRUCTURAL COMPONENTS); STIFFNESS MATRIX;

WINGS;

EID: 34247110840     PISSN: 02734508     EISSN: None     Source Type: Conference Proceeding    
DOI: None     Document Type: Conference Paper

References (10)

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