Force and Moment Test on a Low Boom Configuration in Glenn's 8 x 6 Wind Tunnel (Invited)-Reference-Cited by-同舟云学术

登录注册会员服务联系我们

Force and Moment Test on a Low Boom Configuration in Glenn's 8 x 6 Wind Tunnel (Invited)

Published:2011-06-27 Issue: Volume: Page:
ISSN:
Container-title:29th AIAA Applied Aerodynamics Conference
language:
Short-container-title:

Author:

Wayman Thomas¹,Hicks G.¹,Merret Jason¹

Affiliation:

1. Gulfstream Aerospace Corporation

Publisher

American Institute of Aeronautics and Astronautics

Link

http://arc.aiaa.org/doi/pdf/10.2514/6.2011-3332

Reference9 articles.

1. Henne,P."TheCaseforSmallSupersonicCivilAircraft,"AIAA2003-2555,2003.

2. Henne,P.A.,Howe,D.C.,Wolz,R.R.,andHancock,J.L.,GulfstreamAerospaceCorporation,Savannah,GA, U.S. Patent for a "Supersonic Aircraft withSpike for Controllingand ReducingSonic Boom," Patent No. US 6,698,684 B1, March2,2004.

3. Howe,D.C."ImprovedSonicBoomMinimizationwithExtendableNoseSpike",AIAA-2005-1014.

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

1. Feasibility of Supersonic Aircraft Concepts for Low-Boom and Flight Trim Constraints;33rd AIAA Applied Aerodynamics Conference;2015-06-19

2. Flight Dynamics Modeling of a Supersonic Aircraft Concept;53rd AIAA Aerospace Sciences Meeting;2015-01-02

3. USM3D Analysis of Low Boom Configuration (Invited);29th AIAA Applied Aerodynamics Conference;2011-06-27

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