Six sigma robust design optimization for thermal protection system of hypersonic vehicles based on successive response surface method-Reference-Cited by-同舟云学术

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Six sigma robust design optimization for thermal protection system of hypersonic vehicles based on successive response surface method

Published:2019-09 Issue:9 Volume:32 Page:2095-2108
ISSN:1000-9361
Container-title:Chinese Journal of Aeronautics
language:en
Short-container-title:Chinese Journal of Aeronautics

Author:

ZHU Jingjing,WANG Xiaojun,ZHANG Haiguo,LI Yuwen,WANG Ruixing,QIU Zhiping

Funder

National Key Research and Development Program

National Nature Science Foundation of China

Defence Industrial Technology Development Programs

Publisher

Elsevier BV

Subject

Mechanical Engineering,Aerospace Engineering

Reference48 articles.

1. Theoretical prediction of thermal conductivity for thermal protection systems;Gori;Appl Therm Eng,2012

2. Optimization design of built-up thermal protection system based on validation of corrugated core homogenization;Ma;Appl Therm Eng,2017

3. Calculation of high-temperature insulation parameters and heat transfer behaviors of multilayer insulation by inverse problems method;Huang;Chin J Aeronaut,2014

4. Sun J, Zhang G, Vlahopoulos N, Hong SB. Multi-Disciplinary design optimization under uncertainty for thermal protection system applications. 11th AIAA/ISSMO multidisciplinary analysis and optimization conference; 2006 Sep 6–8; Virginia, USA. Reston: AIAA; 2006. p. 1–14.

5. Thermo-structural optimization of integrated thermal protection panels with one-layer and two-layer corrugated cores based on simulated annealing algorithm;Zhao;Struct Multidiscip Optim,2014

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