Airfoil design method using the Navier-Stokes equations
Author:
Affiliation:
1. NASA Langley Research Center, Hampton, Virginia 23665
2. Bell Helicopter Textron, Inc., Ft. Worth, Texas 76101
3. Georgia Institute of Technology, Atlanta, Georgia 30332
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Aerospace Engineering
Link
http://arc.aiaa.org/doi/pdf/10.2514/3.46015
Reference26 articles.
1. A combined direct/inverse three-dimensional transonic wing design method for vector computers
2. Iterative three-dimensional transonic wing design using integral equations
Cited by 43 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. Inverse aerodynamic design for distributed propulsion wing with expected circulation distribution;Chinese Journal of Aeronautics;2024-05
2. A novel deep-learning-based pressure distribution prediction approach of airfoils;Proceedings of the Institution of Mechanical Engineers, Part G: Journal of Aerospace Engineering;2023-10-19
3. Optimization of Low Reynolds number airfoil design using Full Inverse Design method;2023-06-05
4. Shape Optimization of an Asymmetric Airfoil for Low Wind Speed Region having Adjoint-Based Optimization Technique;Journal of Applied Fluid Mechanics;2023-02-01
5. Development and validation of a hybrid aerodynamic design method for curved diffusers using genetic algorithm and ball-spine inverse design method;Alexandria Engineering Journal;2021-06
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