Nonlinear Aerodynamic Model for Wings in Dynamic Ground Effect
Author:
Affiliation:
1. Simón Bolívar University, Naiguatá, La Guaira 1160, Venezuela
2. Aeronautics Institute of Technology, 12228-900 São José dos Campos, São Paolo, Brazil
3. Simón Bolívar University, Caracas 1080-A, Venezuela
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Aerospace Engineering
Reference21 articles.
1. Stability of airplanes in ground effect
2. Experimental and Analytic Investigation of Ground Effect
3. Dynamic ground effects on a two-dimensional flat plate
4. Dynamic Ground Effect on the Aerodynamic Coefficients Using a Panel Method
5. EtkinB., Dynamics of Atmospheric Flight, Wiley, New York, 1972, pp. 162–163, 285–286.
Cited by 5 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. Determination and analysis of roll and yaw rotary derivatives of wig vehicle using numerical simulation;Aerospace Systems;2022-11-28
2. Nonlinear Aerodynamic Model in Dynamic Ground Effect at High Angles of Attack;Journal of Aircraft;2022-11
3. Numerical simulation of wake vortex for the flight near the ground with different boundary conditions;Engineering Applications of Computational Fluid Mechanics;2022-02-06
4. Stall in ground effect using the unsteady vortex lattice method with Kirchhoff-based correction;ADV AIRCR SPACECR SC;2021
5. Preliminary Design of Aircraft without Vertical Tail;IOP Conference Series: Earth and Environmental Science;2021-02-01
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