Optimization of helicopter rotor blade performance by spline-based taper distribution using neural networks based on CFD solutions
Author:
Affiliation:
1. Aerospace Engineering, Ankara Yildirim Beyazit University, Ankara, Turkey
Publisher
Informa UK Limited
Subject
Modeling and Simulation,General Computer Science
Link
https://www.tandfonline.com/doi/pdf/10.1080/19942060.2019.1648322
Reference32 articles.
1. An unsteady multiblock multigrid scheme for lifting forward flight rotor simulation
2. CFD-based optimization of hovering rotors using radial basis functions for shape parameterization and mesh deformation
3. Developing an ANFIS-based swarm concept model for estimating the relative viscosity of nanofluids
4. Caradonna, F. X. & Tung, C. (1981). Experimental and analytical studies of a model helicopter rotor in hover (NASA Technical Memorandum 81232). Army Aeromechanics Laboratory’s hover test facility.
5. Numerical solutions of forward-flight rotor flow using an upwind method
Cited by 13 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. Twist Optimization of a Helicopter Rotor Blade Using Support Vector Regression;AIAA AVIATION 2023 Forum;2023-06-08
2. Low-Fidelity Aerodynamic Load Analysis of Helicopter Rotor in Hover *;J AERONAUT ASTRONAUT;2023
3. Learning radar cross section of an intermeshing-rotor helicopter with blade pitch;Aircraft Engineering and Aerospace Technology;2023-04-20
4. A new blade tip geometry to improve aerodynamic performance and acoustic noise of helicopter blade in hovering flight;Aerospace Science and Technology;2023-04
5. Application of Leading-Edge Tubercles on Rotor Blades;AIAA Journal;2023-01
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