Influence of high fidelity structural models on the predicted mass of aircraft wing using design optimization-Reference-Cited by-同舟云学术

登录注册会员服务联系我们

Influence of high fidelity structural models on the predicted mass of aircraft wing using design optimization

Published:2018-08 Issue: Volume:79 Page:164-173
ISSN:1270-9638
Container-title:Aerospace Science and Technology
language:en
Short-container-title:Aerospace Science and Technology

Author:

Dababneh Odeh,Kipouros Timoleon

Publisher

Elsevier BV

Subject

Aerospace Engineering

Reference51 articles.

1. Aircraft Design: A Conceptual Approach;Raymer,2006

2. Airplane Design: Part III – Layout Design of Cockpit, Fuselage, Wing and Empennage: Cutaways and Inboard Profiles;Roskam,1989

3. Synthesis of Subsonic Airplane Design;Torenbeek,1982

4. FAME-liA 4. 00 F3 – Validation Document;Ediger,2004

5. Parametric set-up of a structural model for FERMAT configuration for aeroelastic and loads analysis;Klimmek;Aeroelast. Struct. Dyn. J.,2014

Cited by 18 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. Component-based wing structure reconfiguration and analysis on the fly;Aerospace Science and Technology;2024-08

2. An integrated optimization method of multi-hierarchy variables for rudder structures with radial force transfer paths;Aerospace Science and Technology;2024-05

3. Space deployable mechanics: A review of structures and smart driving;Materials & Design;2024-01

4. Component-Based Aircraft Wing Structure Reconfiguration and Analysis on the Fly;2024

5. Component-Based Aircraft Wing Structure Reconfiguration and Analysis on the Fly;2024

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