首页> 外文OA文献 >Correction: Co-design of an Integrated Direct-drive Electric Motor and Propeller for Aircraft Propulsion

【2h】

Correction: Co-design of an Integrated Direct-drive Electric Motor and Propeller for Aircraft Propulsion

机译：校正：共同设计集成的直接驱动电动机和用于飞机推进器的螺旋桨

代理获取

本网站仅为用户提供外文OA文献查询和代理获取服务，本网站没有原文。下单后我们将采用程序或人工为您竭诚获取高质量的原文，但由于OA文献来源多样且变更频繁，仍可能出现获取不到、文献不完整或与标题不符等情况，如果获取不到我们将提供退款服务。请知悉。

页面导航

著录项
引文网络
相似文献
相关主题

著录项

作者
Thanatheepan Balachandran; John Reband; Jianqiao Xiao; Samith Srimmana; Kiruba S. Haran;
展开▼
作者单位

展开▼
年度 2020
总页数
原文格式 PDF
正文语种
中图分类

相似文献

外文文献
中文文献
专利

1. Application of Direct-Drive Wheel Motor for Fuel Cell Electric and Hybrid Electric Vehicle Propulsion System [J] . Rahman K.M., Patel N.R., Ward T.G., IEEE Transactions on Industry Applications . 2006,第期

机译：直驱轮式电动机在燃料电池和混合动力汽车推进系统中的应用
2. Co-design of aircraft vertical tail and control laws with distributed electric propulsion and flight envelop constraints [J] . Eric Nguyen Van, Daniel Alazard, Carsten Doell, CEAS Aeronautical Journal . 2021,第1期

机译：飞机垂直尾部和控制法的共同设计，具有分布式电动推进和飞行信封限制
3. Co-design of aircraft vertical tail and control laws using distributed electric propulsion * [J] . E. Nguyen Van, D. Alazard, C. D?ll, IFAC PapersOnLine . 2019,第12期

机译：使用分布式电力推进技术共同设计飞机垂直尾翼和控制律 *
4. Co-design of an Integrated Direct-drive Electric Motor and Ducted Propeller for Aircraft Propulsion [C] . Thanatheepan Balachandran, John David Reband, Jianqiao Xiao, AIAA/IEEE Electric Aircraft Technologies Symposium . 2020

机译：飞机推进器集成直驱电动机和风道螺旋桨的联合设计
5. Electric propulsion with emphasis on switched reluctance motors and the motor optimum speed ratio. [D] . Hall Mitre, Edilberto. 2002

机译：电动推力，重点放在开关磁阻电动机和电动机最佳转速比上。
6. Publisher Correction: Recent progress and perspectives of space electric propulsion systems based on smart nanomaterials [O] . I. Levchenko, S. Xu, G. Teel, -1

机译：出版商更正：基于智能纳米材料的空间电力推进系统的最新进展和前景
7. An Energy Efficiency Optimization Method for Fixed Pitch Propeller Electric Aircraft Propulsion Systems [O] . Shuli Wang, Shuo Zhang, Shaohua Ma 2019

机译：固定间距螺旋桨电气飞机推进系统的能效优化方法
8. Power Requirements Determined for High-Power-Density Electric Motors for Electric Aircraft Propulsion [R] . Johnson, Dexter, Brown, Gerald V. 2005

机译：用于电动飞机推进的高功率密度电动机的功率要求

Correction: Co-design of an Integrated Direct-drive Electric Motor and Propeller for Aircraft Propulsion

著录项

引文网络

相似文献

相关主题

期刊订阅