With more efficient structures, last trends in aeronautics have witnessed an increased flexibility of wings, calling for adequate design and optimization approaches. To correctly model the coupled physics, aerostructural optimization has progressively become more important, being nowadays performed also considering higher-fidelity discipline methods, i.e., CFD for aerodynamics and FEM for structures. In this work a model for high-fidelity gradient-based aerostructural optimization of wings, assisted by algorithmic differentiation and including aerodynamic and structural nonlinearities, is presented. First, the model is illustrated: a key feature lies in its enhanced modularity. Each discipline solver, employing algorithmic differentiation f...
AbstractMultidisciplinary analysis is necessary to reach physically meaningful optimum designs. For ...
Although the aerospace sector is currently responsible for a relatively small portion of global anth...
As contemporary aerostructural research for aircraft design trends toward high-fidelity computationa...
Gradient based methods in multidisciplinary optimization are promising to exploit remaining potentia...
This thesis is motivated by the desire to discover fuel efficient aircraft concepts through explorat...
Gradient-based aero-structural optimization strategies using high-fidelity CFD methods and close-to-...
Peer Reviewedhttp://deepblue.lib.umich.edu/bitstream/2027.42/83549/1/AIAA-2010-9231-250.pd
International audienceAerostructural optimization is a keystone process to concurrently improve aero...
Aerodynamic shape optimization of a common airliner elastic wing is presented and compared with opti...
This paper presents a method for simultaneous optimization of the outer shape and internal topology ...
Advances in numerical optimization have raised the possibility that efficient and novel aircraft con...
International audienceThis paper presents the current developments performed at ONERA to extend the ...
This thesis presents new tools and techniques developed to address the challenging problem of high-f...
This paper presents a method for wing aerostructural analysis and optimization, which needs much low...
Novel aircraft concepts employing ultrahigh-aspect-ratio wings, such as the strut-braced wing (SBW) ...
AbstractMultidisciplinary analysis is necessary to reach physically meaningful optimum designs. For ...
Although the aerospace sector is currently responsible for a relatively small portion of global anth...
As contemporary aerostructural research for aircraft design trends toward high-fidelity computationa...
Gradient based methods in multidisciplinary optimization are promising to exploit remaining potentia...
This thesis is motivated by the desire to discover fuel efficient aircraft concepts through explorat...
Gradient-based aero-structural optimization strategies using high-fidelity CFD methods and close-to-...
Peer Reviewedhttp://deepblue.lib.umich.edu/bitstream/2027.42/83549/1/AIAA-2010-9231-250.pd
International audienceAerostructural optimization is a keystone process to concurrently improve aero...
Aerodynamic shape optimization of a common airliner elastic wing is presented and compared with opti...
This paper presents a method for simultaneous optimization of the outer shape and internal topology ...
Advances in numerical optimization have raised the possibility that efficient and novel aircraft con...
International audienceThis paper presents the current developments performed at ONERA to extend the ...
This thesis presents new tools and techniques developed to address the challenging problem of high-f...
This paper presents a method for wing aerostructural analysis and optimization, which needs much low...
Novel aircraft concepts employing ultrahigh-aspect-ratio wings, such as the strut-braced wing (SBW) ...
AbstractMultidisciplinary analysis is necessary to reach physically meaningful optimum designs. For ...
Although the aerospace sector is currently responsible for a relatively small portion of global anth...
As contemporary aerostructural research for aircraft design trends toward high-fidelity computationa...