Six sigma robust design optimization for thermal protection system of hypersonic vehicles based on successive response surface method
accepted 3 January 2019Available online 30 May 2019?2019 Chinese Society of Aeronautics and Astronautics. Production and hosting by Elsevier Ltd. This is an open access article under the CC BY-NC-ND license (http://creativecommons.org/licenses/by-nc-nd/4.0/).
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2019-11-08(万方平台首次上网日期,不代表论文的发表时间)
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2095-2108