Structural optimization of a hat stiffened panel by response surface techniques-Reference-Cited by-同舟云学术

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Structural optimization of a hat stiffened panel by response surface techniques

Published:1997-04-07 Issue: Volume: Page:
ISSN:
Container-title:38th Structures, Structural Dynamics, and Materials Conference
language:
Short-container-title:

Author:

Vitali Roberto¹,Vitali Roberto¹,Park Oung¹,Haftka Raphael¹,Sankar Bhavani¹,Park Oung¹,Haftka Raphael¹,Sankar Bhavani¹

Affiliation:

1. Florida, Univ., Gainesville

Publisher

American Institute of Aeronautics and Astronautics

Link

http://arc.aiaa.org/doi/pdf/10.2514/6.1997-1151

Reference6 articles.

1. NASA Contracts NAS1 18862, 20014 and 20546.

2. Panda—Interactive program for minimum weight design of stiffened cylindrical panels and shells

Cited by 8 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. Issues in Deciding Whether to Use Multifidelity Surrogates;AIAA Journal;2019-05

2. Multi-fidelity optimization of laminated conical shells for buckling;Structural and Multidisciplinary Optimization;2005-03-18

3. Bilevel Design of a Wing Structure Using Response Surfaces;Journal of Aircraft;2003-09

4. Evolutionary Optimization for Simultaneous Design on Supersonic Flutter and Structural Mass;9th AIAA/ISSMO Symposium on Multidisciplinary Analysis and Optimization;2002-09-04

5. Structural Optimization of a Hat-Stiffened Panel Using Response Surfaces;Journal of Aircraft;2002-01

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