Results 91 to 100 of about 224,566 (258)
Progressive construction of a parametric reduced-order model for PDE-constrained optimization [PDF]
An adaptive approach to using reduced-order models as surrogates in PDE-constrained optimization is introduced that breaks the traditional offline-online framework of model order reduction.
Farhat, Charbel, Zahr, Matthew J.
core
Manifold Learning for Aerodynamic Shape Design Optimization
The significant computational cost incurred due to the iterative nature of Computational Fluid Dynamics (CFD) in traditional aerodynamic shape design frameworks poses a major challenge, especially in the context of modern integrated design requirements ...
Boda Zheng +3 more
doaj +1 more source
Multi-disciplinary robust design of variable speed wind turbines [PDF]
This paper addresses the preliminary robust multi-disciplinary design of small wind turbines. The turbine to be designed is assumed to be connected to the grid by means of power electronic converters.
Campobasso, Michele Sergio +4 more
core
A New Cokriging Method for Variable-Fidelity Surrogate Modeling of Aerodynamic Data [PDF]
Cokriging is a statistical interpolation method for the enhanced prediction of a less intensively sampled primary variable of interest with assistance of intensively sampled auxiliary variables. In the geostatistics community it is referred to as two- or
Görtz, Stefan +2 more
core +1 more source
The wing aerodynamic shape optimization is a typical high-dimensional problem with numerous independent design variables. Researching methods to reduce the dimensionality of optimization from the perspective of aerodynamic characteristics is necessary ...
Boqian Ji +4 more
doaj +1 more source
Considering the influence of high-speed obstacle avoidance trajectory in the optimization design stage of intelligent bus aerodynamic shape. A collaborative optimization method aiming at aerodynamic structure and trajectory control system for intelligent
Tingting Wang +5 more
doaj +1 more source
Aerodynamic Optimization Design of the Rotor Blade of a Tilt-rotor Aircraft
The aerodynamic design of tilt-rotor needs to synthetically consider the different requirements in helicopter mode and fixed-wing aircraft mode. The multi-objective genetic algorithm based on Kriging surrogate model is used to establish an optimization ...
Sun Kaijun +3 more
doaj +1 more source
Aerodynamic shape optimization based on discrete adjoint and RBF
L. Abergo, M. Morelli, A. Guardone
semanticscholar +1 more source
Most existing studies on aerodynamic shape optimization have not considered longitudinal trim under control surface deflection, typically achieving self-trim through a constraint of zero pitching moment or adjusting the optimized configuration for ...
Yacong Wu +3 more
doaj +1 more source

