Complete Configuration Aero-Structural Optimization Using a Coupled Sensitivity Analysis Method
9th AIAA/ISSMO Symposium on Multidisciplinary Analysis and Optimization
2002-01-01
Conference paper
Electronic Resource
English
business jet , structural displacements , aircraft configurations , finite-element model , drag coefficients , empennage , Structural Optimization , numerical optimization , drag coefficient , sensitivity analysis , nacelles , wing box , structural optimization , freestream , aerodynamic shape optimization , aerodynamics , structural design , optimization algorithm , fuselage , Sensitivity Analysis , structural element , structural weight , lift distribution , aircraft configuration , finite element model , Euler equations , wave drag , structural finite elements , aerodynamic loads , structural analysis , Mach numbers , Fuselage , aerodynamic design , structural finite element
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