Frequency response of an aircraft wing with discrete source damage using equivalent plate analysis

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

Volumn 5, Issue , 2007, Pages 5274-5291

  Krishnamurthy, T ^a,c,d   Eldred, Lloyd B ^b,c,d  

^a NASA LANGLEY RESEARCH CENTER   (United States)

^b Vehicle Analysis Branch   (United States)

^c MS 188E   (United States)

^d AIAA   (United States)

Author keywords

[No Author keywords available]

Indexed keywords

AIRCRAFT MODELS; COMPUTATIONAL EFFICIENCY; DAMAGE DETECTION; FREQUENCY RESPONSE; NATURAL FREQUENCIES; PLATES (STRUCTURAL COMPONENTS);

DISCRETE SOURCE DAMAGE; EQUIVALENT PLATE ANALYSIS; FLIGHT VEHICLE WINGS; STIFFNESS-MATCHED PLATES;

WINGS;

EID: 34547541200     PISSN: 02734508     EISSN: None     Source Type: Conference Proceeding    
DOI: 10.2514/6.2007-2144     Document Type: Conference Paper

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