Aerospace Computing & Design Lab

Motion Estimation and Hand Gesture Recognition-Based Human–UAV Interaction Approach in Real Time. (2022). Yoo, M., Na, Y., Song, H., Kim, G., Yun, J., Kim, S., Moon, C., & Jo, K. Sensors, 22(7), 2513. doi:10.3390/s22072513

Estimation and Separation of Longitudinal Dynamic Stability Derivatives with Forced Oscillation Method Using Computational Fluid Dynamics. (2021). Juliawan, N., Chung, H.-S., Lee, J.-W., & Kim, S. Aerospace, 8(11), 354. doi:10.3390/aerospace8110354

Enhancement of light aircraft 6 DOF simulation using flight test data in longitudinal motion. (2021). Nguyen, L. V. T., Tyan, M., Lee, J.-W., & Kim, S. The Aeronautical Journal, 125(1290), 1358–1379. doi:10.1017/aer.2021.18

Multistage liquid rocket weight estimation and optimization for early design stages. (2020). Shu, J. I., Lee, J. W., Kim, S., Lee, J. L., & Wang, Y. Journal of Aerospace Engineering, 33(6), 04020069. doi:10.1061/(ASCE)AS.19435525.0001181

Design-airworthiness integration method for general aviation aircraft during early development stage. (2019). Tyan, M., Yoon, J., Nguyen, N. V., Lee, J. W., & Kim, S. Aircraft Engineering and Aerospace Technology, 91(7), 1067-1076. doi:10.1108/aeat-05-2018-0143

Efficient approach to database integration for an aerospace vehicle design and certification framework. (2018). Maw, A. A., Lwin, T., Tyan, M., Lee, J. W., & Kim, S. Advances in Engineering Software, 118, 27-34. doi:10.1016/j.advengsoft.2018.01.001

Comprehensive preliminary sizing/resizing method for a fixed wing–VTOL electric UAV. (2017). Tyan, M., Van Nguyen, N., Kim, S., & Lee, J. W. Aerospace Science and Technology, 71, 30-41. doi:10.1016/j.ast.2017.09.008

Process of establishing design requirements and selecting alternative configurations for conceptual design of a VLA. (2017). Bae, B. Y., Kim, S., Lee, J. W., Van Nguyen, N., & Chung, B. C. Chinese Journal of Aeronautics, 30(2), 738-751. doi:10.1016/j.cja.2017.02.018

Database adaptive fuzzy membership function generation for possibility-based aircraft design optimization. (2017). Tyan, M., Nguyen, N. V., Kim, S., & Lee, J. W. Journal of Aircraft, 54(1), 114-124. doi:10.2514/1.C033833

Efficient stall compliance prediction method for trimmed very light aircraft with high-lift devices. (2017). Van Nguyen, N., Lee, D., Tyan, M., Lee, J. W., & Kim, S. Proceedings of the Institution of Mechanical Engineers, Part G: Journal of Aerospace Engineering, 231(6), 1124-1137. doi:10.1177/0954410016648981

Enhanced multi-fidelity model for flight simulation using global exploration and the Kriging method. (2017). Lee, D., Van Nguyen, N., Tyan, M., Chun, H. G., Kim, S., & Lee, J. W. Proceedings of the Institution of Mechanical Engineers, Part G: Journal of Aerospace Engineering, 231(4), 606-620. doi:10.1177/0954410016641441

Investigations on stability and control characteristics of a CS-VLA certified aircraft using wind tunnel test data. (2016). Van Nguyen, N., Tyan, M., Lee, J. W., & Kim, S. Proceedings of the Institution of Mechanical Engineers, Part G: Journal of Aerospace Engineering, 230(14), 2728-2743. doi:10.1177/0954410016632016

Multidisciplinary mission design optimization for space launch vehicles based on sequential design process. (2016). Shu, J. I., Kim, J. W., Lee, J. W., & Kim, S. Proceedings of the Institution of Mechanical Engineers, Part G: Journal of Aerospace Engineering, 230(1), 3-18. doi:10.1177/0954410015586858

Repetitively enhanced neural networks method for complex engineering design optimisation problems. (2015). Van Nguyen, N., Lee, J. W., Tyan, M., & Kim, S. The Aeronautical Journal, 119(1220), 1253-1270. doi:10.1017/S0001924000011234

Aircraft Design Optimization Process using a Decision Model by Database. (2015). Naing, H. M., Van Nguyen, N., Lee, J. W., & Kim, S. Transactions of the Japan Society for Aeronautical and Space Sciences, 58(1), 30-38. doi:10.2322/tjsass.58.30

Multidisciplinary unmanned combat air vehicle system design using multi-fidelity model. (2013). Nguyen, N. V., Choi, S. M., Kim, W. S., Lee, J. W., Kim, S., Neufeld, D., & Byun, Y. H. Aerospace Science and Technology, 26(1), 200-210. doi:10.1016/j.ast.2012.04.004

Automated generation of aerofoil characteristics for rotorcraft application. (2012). Vu, N. A., Lee, J. W., Kim, S., & Neufeld, D. Aircraft Engineering and Aerospace Technology: An International Journal, 84(4), 221-230. doi:10.1108/00022661211237746

Configuration design and optimisation study of a compound gyroplane. (2011). Anh Vu, N., Lee, Y. J., Lee, J. W., Kim, S., & Jae Chung, I. Aircraft Engineering and Aerospace Technology, 83(6), 420-428. doi:10.1108/00022661111173298

Enhancement of class of adjoint design methods via optimization of parameters.(2010). Kim, S., Hosseini, K., Leoviriyakit, K., & Jameson, A. (2010). AIAA journal, 48(6), 1072-1076. doi:10.2514/1.42985

A systematic approach for quantitative analysis of multidisciplinary design optimization framework. (2010). Kim, S., Park, J., Lee, J. O., & Lee, J. W. Transactions of the Japan Society for Aeronautical and Space Sciences, 52(178), 246-254. doi:10.2322/tjsass.52.246

Asymmetric vortices around a body at high angle of attack supersonic flow. (2009). Kim, S. H., & Kim, W. Journal of the Korean Physical Society, 55(5), 2159-2165. doi:10.3938/jkps.55.2159

A problem solving environment portal for multidisciplinary design optimization. (2009). Kim, J. H., Lee, H. J., Kim, S. H., & Lee, J. O. Advances in Engineering Software, 40(8), 623-629. doi:10.1016/j.advengsoft.2008.11.006

Multiobjective optimization using adjoint gradient enhanced approximation models for genetic algorithms. (2006, May). Kim, S., & Chung, H. S. In International Conference on Computational Science and Its Applications (pp. 491-502). Berlin, Heidelberg: Springer Berlin Heidelberg. doi:10.1007/11751649_54

A Framework for Coupling Reynolds-Averaged With Large-Eddy Simulations for Gas Turbine Applications. (2005). Schlüter, J. U., Wu, X., Kim, S., Shankaran, S., Alonso, J. J., & Pitsch, H. ASME. J. Fluids Eng. 127(4). 806–815. doi:10.1115/1.1994877

Multi-element high-lift configuration design optimization using viscous continuous adjoint method.A Framework for Coupling Reynolds-Averaged With Large-Eddy Simulations for Gas Turbine Applications. (2005). Kim, S., Alonso, J. J., & Jameson, A. Journal of Aircraft, 41(5), 1082-1097. doi:10.2514/1.17

Reduction of the adjoint gradient formula for aerodynamic shape optimization problems. (2003). Jameson, A., & Kim, S. AIAA journal, 41(11), 2114-2129. doi:10.2514/2.6830