실험비용을 고려한 적응적 실험설계법 기반 KF-16 피칭모멘트계수 모델링 Pitching Moment Coefficient Modeling of KF-16 using Adaptive Design of Experiments with cost consideration

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A new approach to systematically model aerodynamic coefficients using an adaptive sampling based wind tunnel testing considering cost is proposed. The Latin Hypercube design is used for selecting initial test points. The Gaussian Process (GP) is iteratively used during the experiment to determine additional experimental points that minimizes the uncertainty reduction per incremental cost. A numerical simulation based experiment was conducted using the static aerodynamic coefficient database a fighter aircraft, which demonstrated the validity of the proposed method.
Publisher
한국항공우주학회
Issue Date
2016-06
Language
Korean
Article Type
Article
Citation

한국항공우주학회지, v.44, no.6, pp.537 - 543

ISSN
1225-1348
DOI
10.5139/JKSAS.2016.44.6.537
URI
http://hdl.handle.net/10203/213640
Appears in Collection
AE-Journal Papers(저널논문)
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