Structural optimization of a joined wing using equivalent static loads

Journal of Aircraft

Volumn 44, Issue 4, 2007, Pages 1302-1308

  Lee, H A ^a   Kim, Y I ^a   Park, G J ^a   Kolonay, R M ^b   Blair, M ^b   Canfield, R A ^c  

^a Hanyang University   (South Korea)

^b AIR FORCE RESEARCH LABORATORY   (United States)

^c AIR FORCE INSTITUTE OF TECHNOLOGY   (United States)

Author keywords

[No Author keywords available]

Indexed keywords

AERODYNAMICS; COSINE TRANSFORMS; DYNAMIC ANALYSIS; DYNAMIC LOADS; OPTIMIZATION; THICKNESS CONTROL;

AIRPLANE; STATIC LOADS; STRUCTURAL WEIGHT;

WINGS;

EID: 34548351265     PISSN: 00218669     EISSN: 15333868     Source Type: Journal    
DOI: 10.2514/1.26869     Document Type: Article

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