Tilt Duct Vertical Takeoff and Landing Uninhabited Aerial Vehicle Concept Design Study

Author:

Armutcuoglu Ozlem1,Kavsaoglu Mehmet Serif1,Tekinalp Ozan1

Affiliation:

1. Middle East Technical University, 06531 Ankara, Turkey

Publisher

American Institute of Aeronautics and Astronautics (AIAA)

Subject

Aerospace Engineering

Reference33 articles.

1. 1McCormick, B. W., Aerodynamics, Aeronautics and Flight Mechanics, 2nd ed.Wiley, New York, 1995, Chap. 8, pp.432-442.

2. Moving-base simulator study of an all- mechanical control system for vtol aircraft

Cited by 25 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. Preliminary Design and Optimization of Primary Structures for a Tilt-Duct UAV;Aerospace;2024-04-08

2. Conceptual design of long-endurance small solar-powered unmanned aerial vehicle with multiple tilts and hovers;Proceedings of the Institution of Mechanical Engineers, Part G: Journal of Aerospace Engineering;2023-08-18

3. Vertical Take-Off and Landing fixed-wing designed for autonomous missions;2023 IEEE/ASME International Conference on Advanced Intelligent Mechatronics (AIM);2023-06-28

4. Longitudinal flight dynamics modeling and a flight stability analysis of a monocopter;AIP Advances;2022-11-01

5. Conceptual Design and System Level Analysis of Tilt-Duct eVTOL Aircraft;Lecture Notes in Electrical Engineering;2022-08-31

同舟云学术

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