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Stability Derivative Computation of Tailless Aircraft using Variable-Fidelity Aerodynamics Aanlysis
Author
Park, J., Choi, J., Jo, Y., Im, D., and Choi, S.
Year
2017
Source
AIAA Journal of Aircraft, May 2017, https://doi.org/10.2514/1.C034052
Variable-Fidelity Aerodynamic Analysis of Lift Fan Aircraft and Validation
Author
Rachit, P., and Choi, S.
Year
2017
Source
Aerospace Science and Technology (AST), 2017, DOI: 10.1016/j.ast.2017.09.022.
Adaptive Variable-Fidelity Analysis and Design Using Dynamic Fidelity Indicators
Author
Jo, Y., Yi, S., and Choi, S.
Year
2016
Source
AIAA Journal, volume 54, issue 11 pages 3564-3579, October 14, 2016, doi: http://arc.aiaa.org/doi/abs/10.2514/1.J054591
Surrogate model based design optimization of wing sail considering flow interaction effect
Author
Lee, H., Jo, Y., Lee, D., and Choi, S.,
Year
2016
Source
Ocean Engineering, Jun 2016 DOI: 10.1016/j.oceaneng.2016.05.051
Design of an Optimal Route Structure Using Heuristics-Based Stochastic Schedulers
Author
Choi, S., Mulfinger, D., Robinson, J., and Capozzi, B.
Year
2015
Source
Journal of Aircraft, (doi: http://arc.aiaa.org/doi/abs/10.2514/1.C032645)
A Trended Kriging Model with R2 Indicator and Application to Design Optimization
Author
Kwon, H., Yi, S., and Choi, S
Year
2015
Source
Aerospace Science and Technology, , Volume 43, June 2015, Pages 111125 (DOI : 10.1016/j.ast.2015.02.021accepted for publication in 2015)
A Mapped Chebyshev Pseudospectral Method for Unsteady Flow Analysis
Author
Im, D., Choi, S, and McClure, J.
Year
2015
Source
AIAA Journal, Vol. 53, No. 12 (2015), pp. 3805-3820, http://arc.aiaa.org/doi/abs/10.2514/1.J054081
Surrogate-Based Robust Optimization and Design Application to Unsteady Low-Noise Open Rotors
Author
Kwon, H., Choi, S., Lee, D., and Kwon, J.
Year
2015
Source
AIAA J. of Aircraft, Vol. 53, No. 5, pp. 1448-1467
Unsteady Rotor Flow Analysis Using a Diagonally Implicit Harmonic Blance Method and and Overset Mesh Topology
Author
Im, D., Choi, S., and Kwon, J.
Year
2015
Source
International Journal of Computational Fluid Dynamics, Vo. 29, Iss. 1, pp.82–99, http://dx.doi.org/10.1080/10618562.2015.101552
Aerodynamic Design of EAV Propeller Using a Multi-Level Optimization Method
Author
Kwon, H., Yi, S., and Choi, S.
Year
2015
Source
Journal of Propulsion and Power, Vol. 31 Issue. 4, pp 1057-1072, DOI: 10.2514/1.B35097, JulyAugust 2015.
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