Proper Orthogonal Decomposition and Response Surface Method for TPS/RLV Structural Design and Optimization: X-34 Case Study

Author(s):  
Lei Tang ◽  
Ping-Chih Chen ◽  
Danny Liu ◽  
Xiao-Wei Gao ◽  
Wei Shyy ◽  
...  
2021 ◽  
Vol 56 (5) ◽  
pp. 873-884
Author(s):  
Adel Zemirline ◽  
Abdellah Abdellah El Hadj ◽  
Shayfull Z. B. Abd Rahim ◽  
Mohammed Ouali

2014 ◽  
Vol 565 ◽  
pp. 92-97 ◽  
Author(s):  
Jian Yang Li ◽  
Hong Yan Wang ◽  
Qiang Rui ◽  
Huang Jie Hong

The airborne vehicle would suffer from impact at landing. The magnitude of impact and stability of airborne vehicle are constraint parameters of successful landing. There was a lack of scientific explanation on the sensitivity of landing condition parameters. For overcoming the deficiency of classical sensitivity analysis, this paper describes the application of new technology for the sensitivity analysis. Based on the Finite Element and Response Surface method, the research on sensitivity analysis of landing condition parameters was proposed. The results have important significance in the design and optimization of airborne vehicle and airbags system. It can be also provide guidance for airdrop operation.


2014 ◽  
Vol 22 (1) ◽  
pp. 29-35
Author(s):  
Sohyeon Park ◽  
Eunsung Kim ◽  
Sangyeob Oh ◽  
Hyosun Yu ◽  
Sungmo Yang ◽  
...  

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