Effective adjoint approaches for computational fluid dynamics

GKW Kenway, CA Mader, P He… - Progress in Aerospace …, 2019 - Elsevier
The adjoint method is used for high-fidelity aerodynamic shape optimization and is an
efficient approach for computing the derivatives of a function of interest with respect to a …

Multidisciplinary design optimization: a survey of architectures

JRRA Martins, AB Lambe - AIAA journal, 2013 - arc.aiaa.org
Multidisciplinary design optimization is a field of research that studies the application of
numerical optimization techniques to the design of engineering systems involving multiple …

OpenMDAO: An open-source framework for multidisciplinary design, analysis, and optimization

JS Gray, JT Hwang, JRRA Martins, KT Moore… - Structural and …, 2019 - Springer
Multidisciplinary design optimization (MDO) is concerned with solving design problems
involving coupled numerical models of complex engineering systems. While various MDO …

[HTML][HTML] State-of-the-art in aerodynamic shape optimisation methods

SN Skinner, H Zare-Behtash - Applied Soft Computing, 2018 - Elsevier
Aerodynamic optimisation has become an indispensable component for any aerodynamic
design over the past 60 years, with applications to aircraft, cars, trains, bridges, wind …

[HTML][HTML] 汽车轻量化技术的研究现状综述

李光霁, 刘新玲 - 材料科学与工艺, 2020 - hit.alljournals.cn
近年来汽车行业的科技水平发展程度逐渐提高, 汽车行业进入高速发展阶段,
然而随之而来的环境和能源问题也日趋加重. 轻量化技术变成了各个汽车企业提升市场竞争力的 …

Multipoint high-fidelity aerostructural optimization of a transport aircraft configuration

GKW Kenway, JRRA Martins - Journal of Aircraft, 2014 - arc.aiaa.org
This paper presents multipoint high-fidelity aerostructural optimizations of a long-range wide-
body transonic transport aircraft configuration. The aerostructural analysis employs Euler …

Review and unification of methods for computing derivatives of multidisciplinary computational models

JRRA Martins, JT Hwang - AIAA journal, 2013 - arc.aiaa.org
This paper presents a review of all existing discrete methods for computing the derivatives of
computational models within a unified mathematical framework. This framework hinges on a …

Review of output-based error estimation and mesh adaptation in computational fluid dynamics

KJ Fidkowski, DL Darmofal - AIAA journal, 2011 - arc.aiaa.org
Error estimation and control are critical ingredients for improving the reliability of
computational simulations. Adjoint-based techniques can be used to both estimate the error …

Dual-convolutional neural network based aerodynamic prediction and multi-objective optimization of a compact turbine rotor

Y Wang, T Liu, D Zhang, Y Xie - Aerospace Science and Technology, 2021 - Elsevier
With the development of neural network technology, surrogate models and dimensionality
reduction strategies based on machine learning have become the research hotspots of …

Scalable parallel approach for high-fidelity steady-state aeroelastic analysis and adjoint derivative computations

GKW Kenway, GJ Kennedy, JRRA Martins - AIAA journal, 2014 - arc.aiaa.org
Aeroelastic systems achieve the best performance when the aerodynamic shape and
structural sizing are optimized concurrently, but such an optimization is challenging when …