Optimum Design of Stiffened Panels With Substiffeners-Reference-Cited by-同舟云学术

Optimum Design of Stiffened Panels With Substiffeners

Published:2005-04-18 Issue: Volume: Page:
ISSN:
Container-title:46th AIAA/ASME/ASCE/AHS/ASC Structures, Structural Dynamics and Materials Conference
language:
Short-container-title:

Author:

Bushnell David¹,Rankin Charles¹

Affiliation:

1. Rhombus Consultants Group, Inc.

Publisher

American Institute of Aeronautics and Astronautics

Link

http://arc.aiaa.org/doi/pdf/10.2514/6.2005-1932

Reference61 articles.

1. PANDA2—Program for minimum weight design of stiffened, composite, locally buckled panels

2. D. Bushnell,/panda2/doc/panda2.news, a continually updated file distributed with PANDA2 that contains a log of all significant modifications to PANDA2 from 1987 on. In particular, see ITEM No. 600 in that file, which containsmoredetailsaboutthe "substiffener"project.

3. A PRELIMINARY DESIGN PROCEDURE FOR COMPOSITE PANELS WITH OPEN-SECTION STIFFENERS LOADED IN THE POST-BUCKLING RANGE

4. General Panel Sizing Computer Code and Its Application to Composite Structural Panels

Cited by 17 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. Simultaneous isotropic and anisotropic multi-material topology optimization for conceptual-level design of aerospace components;Structural and Multidisciplinary Optimization;2021-03-25

2. Uçak Kanadının Entegre Güçlendirilmiş Panel Yapıları Kullanılarak Yapısal Tasarımı;European Journal of Science and Technology;2020-04-30

3. Experimental and numerical vibration analysis of plates with curvilinear sub-stiffeners;Engineering Structures;2020-04

4. Weight optimization of metal T stiffened panel of a transport aircraft wing using CAE tools;Materials Today: Proceedings;2020

5. Performance and Stability Analysis of Sub-stiffening for Mechanical Buckling and Post Buckling: A Selective Study;MATEC Web of Conferences;2017