Flowfield Prediction of Airfoil Off-Design Conditions Based on a Modified Variational Autoencoder
Author:
Affiliation:
1. Tsinghua University, 100084 Beijing, People’s Republic of China
Funder
National Natural Science Foundation of China
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Aerospace Engineering
Link
https://arc.aiaa.org/doi/pdf/10.2514/1.J061972
Reference32 articles.
1. Data-driven constraint approach to ensure low-speed performance in transonic aerodynamic shape optimization
2. Multipoint and Multi-Objective Aerodynamic Shape Optimization
3. Airfoil Optimization Using Practical Aerodynamic Design Requirements
4. Aerodynamic Shape Optimization Investigations of the Common Research Model Wing Benchmark
5. Multipoint Aerodynamic Shape Optimization Investigations of the Common Research Model Wing
Cited by 10 articles. 订阅此论文施引文献 订阅此论文施引文献，注册后可以免费订阅5篇论文的施引文献，订阅后可以查看论文全部施引文献
1. Transferable machine learning model for the aerodynamic prediction of swept wings;Physics of Fluids;2024-07-01
2. Mesh-Agnostic Decoders for Supercritical Airfoil Prediction and Inverse Design;AIAA Journal;2024-06
3. Uncertainty-Aware Surrogate Models for Airfoil Flow Simulations with Denoising Diffusion Probabilistic Models;AIAA Journal;2024-05-12
4. Fast Buffet-Onset Prediction and Optimization Method Based on Pretrained Flowfield Prediction Model;AIAA Journal;2024-05-12
5. Uncertainty involved drag divergence characteristic predicting method based on VAE;Journal of Membrane Computing;2024-03-26
1.学者识别学者识别
2.学术分析学术分析
3.人才评估人才评估
"同舟云学术"是以全球学者为主线，采集、加工和组织学术论文而形成的新型学术文献查询和分析系统，可以对全球学者进行文献检索和人才价值评估。用户可以通过关注某些学科领域的顶尖人物而持续追踪该领域的学科进展和研究前沿。经过近期的数据扩容，当前同舟云学术共收录了国内外主流学术期刊6万余种，收集的期刊论文及会议论文总量共计约1.5亿篇，并以每天添加12000余篇中外论文的速度递增。我们也可以为用户提供个性化、定制化的学者数据。欢迎来电咨询！咨询电话：010-8811{复制后删除}0370
www.globalauthorid.com
TOP
Copyright © 2019-2024 北京同舟云网络信息技术有限公司 京公网安备11010802033243号 京ICP备18003416号-3