Calculation of blade-vortex interaction airloads on helicopter rotors
Author:
Affiliation:
1. Johnson Aeronautics, Palo Alto, California
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Aerospace Engineering
Link
http://arc.aiaa.org/doi/pdf/10.2514/3.45787
Reference13 articles.
1. Rotor blade harmonic air loading
2. A METHOD FOR COMPUTING ROTARY WING AIRLOAD DISTRIBUTION IN FORWARD FLIGHT
3. Assessment of aerodynamic and dynamic models in a comprehensive analysis for rotorcraft
4. Comparison of Calculated and Measured Helicopter Rotor Lateral Flapping Angles
5. Correlation of SA349/2 Helicopter Flight Test Data with a Comprehensive Rotorcraft Model
Cited by 39 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. Reduction of rotorcraft BVI using synthetic jets; computational studies using LES;International Journal for Computational Methods in Engineering Science and Mechanics;2024-01-29
2. COMPUTATIONAL STUDIES OF HELICOPTER AERODYNAMICS;Annals of the Academy of Romanian Scientists Series on Engineering Sciences;2023
3. Mach number effect on the aeroelastic phenomenon of fixed wing aircraft;AIAA SCITECH 2022 Forum;2022-01-03
4. Computational studies of turbine-stage, with variable inlet temperature; comparison between LES and IDDES;AIAA AVIATION 2021 FORUM;2021-07-28
5. Aerodynamic studies of rotor-stator turbine stage; a computational approach using LES;AIAA Scitech 2020 Forum;2020-01-05
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