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http://dx.doi.org/10.5139/JKSAS.2010.38.11.1067

Reliability Based Design Optimization for the Pressure Recovery of Supersonic Double-Wedge Inlet  

Lee, Chang-Hyuck (한국과학기술원 기계항공시스템학부)
Ahn, Joong-Ki (국방과학연구소)
Bae, Hyo-Gil (한국과학기술원 기계항공시스템학부)
Kwon, Jang-Hyuk (한국과학기술원 기계항공시스템학부)
Publication Information
Journal of the Korean Society for Aeronautical & Space Sciences / v.38, no.11, 2010 , pp. 1067-1074 More about this Journal
Abstract
In this study, RBDO(Reliability Based Design Optimization) was performed for a supersonic double-wedge inlet. By considering uncertainty of design with given design space, the pressure recovery was transformed into the probabilistic constraint while the inlet drag was considered as a deterministic objective function. To save computational analysis cost and to search good design space, Latin-Hypercube design of experiment and the Kriging model were incorporated and then RBDO was performed. Monte-Carlo simulation was performed to verify the accuracy of AFORM(Advanced First Order Reliability Method). It was found that AFORM result agreed very well with the Monte-Carlo simulation result. The system reliability was guaranteed by considering uncertainty of the design variables. In case of considering diverse uncertainty of system design, RBDO was found to be useful.
Keywords
Kriging Model; Design and Analysis of Computer Experiment; Advanced First Order Reliability Method; Reliability Based Design Optimization; Deterministic Design Optimization;
Citations & Related Records
Times Cited By KSCI : 4  (Citation Analysis)
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