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논문명(출판명)
저자
출처
Multi-Objective Optimization of a Node-Based Spacecraft Radiator Design
Author
Kim, H., and Choi, S.
Year
2014
Source
published in Journal of Spacecraft and Rockets, accessed April 15, 2014. doi: http://arc.aiaa.org/doi/abs/10.2514/1.A32763
Helicopter Rotor Design Using a Time-Spectral and Adjoint-Based Method
Author
Choi, S., Lee, K, and Alonso, J.
Year
2014
Source
published in Journal of Aircraft, Vol. 51, Iss. 2, pp. 412–423.
Node-Based Spacecraft Radiator Design Optimization
Author
Kim, H., Choi, S, and S, Park,
Year
2014
Source
Advances in Space Research, ASR, 55 (2015), pp. 1445-1469, DOI:10.1016/j.asr.2014.09.007, Oct 2014.
Numerical investigation for erratic behavior of Kriging surrogate model
Author
Hyungil Kwon, Seulgi Yi, and Seongim Choi
Year
2014
Source
Journal of Mechanical Science and Technology, Vol. 28, Issue 9, pp.3697-3707
Development of an Engineering Education Framework for Aerodynamic Shape Optimization
Author
Hyung-Il Kwon, Saji Kim, Hakjin Lee, Minseok Ryu, Taehee Kim, and Seongim Choi
Year
2013
Source
International Journal of Aeronautical and Space Sciences, Vol.14, No. 4, pp. 297-309
Prediction of Helicopter Rotor Loads Using Time-Spectral Computational Fluid Dynamics and an Exact FluidStructure Interface
Author
Choi, S., Datta, A., and Alonso, J.
Year
2011
Source
published in Journal of American Helicopter Society, Vol. 56, Iss. 4, pp. 042001-1 – 042001-16, 2011
Numerical and Mesh Resolution Requirements for Accurate Sonic Boom Prediction of Complete Aircraft Configurations
Author
Choi, S., and Alonso, J.
Year
2009
Source
published in Journal of Aircraft, Vol. 46, No. 4, pp. 1126-1139, 2009
Two-Level Multi-Fidelity Design Optimization Studies for Supersonic Jets
Author
Choi, S., and Alonso, J.
Year
2009
Source
published in Journal of Aircraft, Vol. 46, No. 3, pp. 776-790, 2009.
Multi-Fidelity Design Optimization of Low-Boom Supersonic Business Jets
Author
Choi, S., Alonso, J., and Kroo, I.
Year
2008
Source
published in Journal of Aircraft, Vol. 45, No. 1, pp. 106-118, 2008.
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