Nonlinear dynamic response structural optimization of a joined-wing using equivalent static loads

Journal of Aircraft

Volumn 46, Issue 3, 2009, Pages 821-831

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

^a Hanyang University   (South Korea)

^b AIR FORCE RESEARCH LABORATORY   (United States)

^c AIR FORCE INSTITUTE OF TECHNOLOGY   (United States)

^d Department of Mechanical Engineering ^*

^e Air Vehicles Directorate   (United States)

Author keywords

[No Author keywords available]

Indexed keywords

AIRCRAFT; ATMOSPHERIC TURBULENCE; DYNAMIC LOADS; DYNAMIC RESPONSE; FINITE DIFFERENCE METHOD; NONLINEAR ANALYSIS; SENSITIVITY ANALYSIS; SHAPE OPTIMIZATION; WINGS;

CONVENTIONAL METHODS; EQUIVALENT STATIC LOADS; EQUIVALENT STATIC LOADS METHODS; GEOMETRIC NON-LINEARITY; JOINED WING CONFIGURATION; LINEAR STATIC ANALYSIS; NONLINEAR STATICS; STRUCTURAL WEIGHT;

STRUCTURAL OPTIMIZATION;

EID: 67650869567     PISSN: 00218669     EISSN: 15333868     Source Type: Journal    
DOI: 10.2514/1.36762     Document Type: Article

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