Surrogate-Based Optimum Design for Stiffened Shells with Adaptive Sampling-Reference-Cited by-同舟云学术

Surrogate-Based Optimum Design for Stiffened Shells with Adaptive Sampling

Published:2012-11 Issue:11 Volume:50 Page:2389-2407
ISSN:0001-1452
Container-title:AIAA Journal
language:en
Short-container-title:AIAA Journal

Author:

Hao Peng¹,Wang Bo¹,Li Gang¹

Affiliation:

1. State Key Laboratory of Structural Analysis for Industrial Equipment, Dalian University of Technology, 116023 Dalian, People's Republic of China

Publisher

American Institute of Aeronautics and Astronautics (AIAA)

Subject

Aerospace Engineering

Link

http://arc.aiaa.org/doi/pdf/10.2514/1.J051522

Reference48 articles.

1. Venkataraman, S. "Modeling, Analysis and Optimization of Cylindrical Stiffened Panels for Reusable Launch Vechicle Structures", Ph.D. Thesis,Department of Mechanical and Aerospace Engineering, Univ. of Florida, Gainesville, FL,1999.

2. Continuous filament wound composite concepts for aircraft fuselage structures

3. Design and Fabrication of CFRP Interstage Attach Fitting for Launch Vehicles

4. Analysis and Optimum Design of Composite Grid Structures

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