Methodology for determining the takeoff mass of all-electric aircraft at the early stages of design
Author:
Publisher
Springer Science and Business Media LLC
Subject
Space and Planetary Science,Computers in Earth Sciences,Mechanical Engineering,Aerospace Engineering,Control and Systems Engineering
Link
https://link.springer.com/content/pdf/10.1007/s42401-023-00242-5.pdf
Reference32 articles.
1. Traub LW (2011) Range and endurance estimates for battery-powered aircraft. J Aircr 48(2):703–707
2. Traub LW (2013) Validation of endurance estimates for battery powered UAVs. Aeronaut J 117(1197):1155–1166
3. Strelets DY, Serebryansky SA, Skurin MV (2019) A digital approach to aircraft product lifecycle management. In: 2019 Twelfth International Conference Management of large-scale system development (MLSD). IEEE
4. Kantimirov S, Serebryansky S (2021) On the issue of weight design of aircraft on a digital platform in a single information space of the product life cycle. In: 2021 14th international conference management of large-scale system development (MLSD). IEEE
5. Dukhnovskiy DA (2020) Formation of the area of possible existence of electrified airplanes. In: 2020 New Trends in Aviation Development (NTAD). IEEE
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