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contributor authorXing, Haifeng
contributor authorLuo, Lei
contributor authorDu, Wei
contributor authorWang, Songtao
date accessioned2022-05-08T08:54:42Z
date available2022-05-08T08:54:42Z
date copyright11/5/2021 12:00:00 AM
date issued2021
identifier issn0889-504X
identifier otherturbo_144_4_041006.pdf
identifier urihttp://yetl.yabesh.ir/yetl1/handle/yetl/4284499
description abstractThe direct prediction model for adiabatic film cooling effectiveness distribution and inverse prediction model for design parameters are studied in this article. Convolutional neural networks (CNNs) are trained on a set of simulated adiabatic film cooling effectiveness contours parameterized by blowing ratio, density ratio, mainstream turbulence intensity, injection angle, and compound angle. The direct model and the inverse model are able to approximate the data in the test set with plausible accuracy. The absolute error of spatial averaged effectiveness no larger than 0.03 could be obtained in the test set by a direct model with time consumption less than 1 ms for a single case. The inverse model is the first model of its kind, which accomplished the inverse mapping from contours to parameters. It has been demonstrated that the concatenation of inverse model with the pretrained direct model, which can be treated as a complex loss function, has preferable approximation performance compared with simple mean squared error (MSE) loss function in the training of the inverse model, thus confirming the necessity of adopting specialized modeling strategies for inverse problems.
publisherThe American Society of Mechanical Engineers (ASME)
titleDirect and Inverse Model for Single-Hole Film Cooling With Machine Learning
typeJournal Paper
journal volume144
journal issue4
journal titleJournal of Turbomachinery
identifier doi10.1115/1.4052601
journal fristpage41006-1
journal lastpage41006-16
page16
treeJournal of Turbomachinery:;2021:;volume( 144 ):;issue: 004
contenttypeFulltext


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