Study of the Influence of Aircraft Geometry on the Computed Flowfield During Thrust Reversers Operation

Author:

Oliveira de Andrade Fernando1,Barros Ferreira Sandro1,Figueira da Silva Luis Fernando1,de Jesus Antonio2,Lara Oliveira Guilherme2

Affiliation:

1. Pontificia Universidade Catolica do Rio de Janeiro

2. EMBRAER

Publisher

American Institute of Aeronautics and Astronautics

Reference11 articles.

1. Performance of a Cascade Thrust Reverser for Short-Haul Applications

2. A Reynolds stress model of turbulence and its application to thin shear flows

3. Solution of an engine inlet compatibility problem during C-17 low cost N/EAT nacelle thrust reverser development

4. Margason, R. J. "The Path of a Jet Directed at a Large Angle to a Subsonic Free Stream," NASA - National Aeronautics and AerospaceAdministration,NASA TND-4919,Nov.1968.

Cited by 3 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

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