Show simple item record

contributor authorChell, Brian
contributor authorHoffenson, Steven
contributor authorPhilippe, Cory J. G.
contributor authorBlackburn, Mark R.
date accessioned2022-02-05T21:47:54Z
date available2022-02-05T21:47:54Z
date copyright2/5/2021 12:00:00 AM
date issued2021
identifier issn1050-0472
identifier othermd_143_8_081702.pdf
identifier urihttp://yetl.yabesh.ir/yetl1/handle/yetl/4276359
description abstractMultifidelity optimization leverages the fast run times of low-fidelity models with the accuracy of high-fidelity models (HFMs), in order to conserve computing resources while still reaching optimal solutions. This work focuses on the multifidelity multidisciplinary optimization of an aircraft system model with finite element analysis and computational fluid dynamics simulations in the loop. A two-step filtering method is used where a lower fidelity model is optimized, and then the solution is used as a starting point for a higher-fidelity optimization routine. By starting the high-fidelity routine at a nearly optimal region of the design space, the computing resources required for optimization are expected to decrease when using local algorithms. Results show that, when using surrogates for the lower fidelity models, the multifidelity workflows save statistically significant amounts of time over optimizing the original HFM alone. However, the impact on solution quality varies depending on the model behavior and optimization algorithm.
publisherThe American Society of Mechanical Engineers (ASME)
titleComparing Filtering Multifidelity Optimization Strategies With a Simulation-Based Multidisciplinary Aircraft Model
typeJournal Paper
journal volume143
journal issue8
journal titleJournal of Mechanical Design
identifier doi10.1115/1.4049657
journal fristpage081702-1
journal lastpage081702-9
page9
treeJournal of Mechanical Design:;2021:;volume( 143 ):;issue: 008
contenttypeFulltext


Files in this item

Thumbnail

This item appears in the following Collection(s)

Show simple item record