STABILITY DERIVATIVE ESTIMATION AT SUBSONIC SPEEDS-Reference-Cited by-同舟云学术

登录注册会员服务联系我们

STABILITY DERIVATIVE ESTIMATION AT SUBSONIC SPEEDS

Published:1968-11 Issue:2 International Volume:154 Page:367-396
ISSN:0077-8923
Container-title:Annals of the New York Academy of Sciences
language:en
Short-container-title:Ann NY Acad Sci

Author:

Ellison Don E.,Hoak Donald E.

Publisher

Wiley

Subject

History and Philosophy of Science,General Biochemistry, Genetics and Molecular Biology,General Neuroscience

Link

http://onlinelibrary.wiley.com/wol1/doi/10.1111/j.1749-6632.1968.tb15207.x/fullpdf

Reference97 articles.

1. 1. D. E. ELLISON, and L. V. MALTHAN . 1960 . (Rev.1960 , 1960 ). USAF Stability and Control Datcom.

2. 4. D. B. BENEPE, B. G. KOURI, and J. B. WEBB, 1966 . Aerodynamic characteristics of non-straight-taper wings. AFFDL-TR-66-73.

3. 5. T. TOLL, and M. QUEIJO . 1948 . Approximate relations and charts for low-speed stability and control derivatives of swept wings. NACA TN 1581.

Cited by 5 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. Generic Characterisation of Aircraft—Parameter Reduction Process;Stability and Control of Conventional and Unconventional Aerospace Vehicle Configurations;2019

2. A Vortex-Lattice Method for Calculating Longitudinal Dynamic Stability Derivatives of Oscillating Delta Wings;AIAA Journal;1984-01

3. Preliminary tailplane design;Synthesis of Subsonic Airplane Design;1982

4. Preliminary tailplane design;Synthesis of subsonic airplane design;1976

5. Analysis of aerodynamic and operational characteristics;Synthesis of subsonic airplane design;1976

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