Optimization of a morphing wing based on coupled aerodynamic and structural constraints

AIAA Journal

Volumn 47, Issue 9, 2009, Pages 2087-2104

  Gamboa, P ^a,d   Vale, J ^b,e   Lau, F J P ^b,e   Suleman, A ^c,e  

^a UNIVERSITY OF BEIRA INTERIOR   (Portugal)

^b INSTITUTO SUPERIOR TÉCNICO   (Portugal)

^c UNIVERSITY OF VICTORIA   (Canada)

^d Aerospace Sciences Department   (Portugal)

^e Mechanical Engineering Department   (Canada)

Author keywords

[No Author keywords available]

Indexed keywords

AERODYNAMIC SHAPE OPTIMIZATION; COUPLED AERODYNAMICS; FIXED WING; FLIGHT SPEED; MECHANISM DESIGN; MORPHING; MORPHING WINGS; MULTIDISCIPLINARY DESIGN OPTIMIZATION; OPTIMIZATION ALGORITHMS; OPTIMIZATION PROCEDURES; PANEL METHODS; PERFORMANCE ENHANCEMENTS; SEQUENTIAL QUADRATIC PROGRAMMING; SPEED RANGE; STRUCTURAL CONSTRAINTS; STRUCTURAL MODELS; WING DESIGN;

AERODYNAMIC DRAG; AERODYNAMICS; COMBINATORIAL OPTIMIZATION; FIXED WINGS; MACHINE DESIGN; MODEL STRUCTURES; MULTI AGENT SYSTEMS; OPTIMAL SYSTEMS; QUADRATIC PROGRAMMING; REMOTELY OPERATED VEHICLES; UNMANNED AERIAL VEHICLES (UAV);

SHAPE OPTIMIZATION;

EID: 73649084464     PISSN: 00011452     EISSN: None     Source Type: Journal    
DOI: 10.2514/1.39016     Document Type: Article

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