International Conference

[17] Yeongmin Jo, Thierry Jardin, Romain Gojon, Marc. C. Jacob, and Jean-Marc Moschetta, “Parametric Study of Low Noise Rotor for MAV at Unsteady Low Reynolds Number Flow,” AIAA/CEAS 2019, May 20-24, 2019. (https://doi.org/10.2514/6.2019-2615)

[16] Yeongmin Jo, Hakjin Lee, and Duck-Joo Lee, “Prediction of Rotor Flow for Unmanned Aerial System Using Nonlinear Vortex Lattice Method,” 6th Asia/Austrailian Rotorcraft Forum / Heli Japan 2017, Kanazawa, Japan, Nov. 7-9, 2017.

[15] Hakjin Lee, Yeongmin Jo, and Duck-Joo Lee, “Development of Nonlinear Vortex Lattice Method and Its Application to Aerodynamic Analysis of Wind Turbine,” 6th Asia/Australian Rotorcraft Forum / Heli Japan 2017, Kanazawa, Japan, Nov. 7-9, 2017.

[14] Jangho Park, Yeongmin Jo, Seulgi Yi, Seongim Choi, and Pradeep Raj, “Variable-Fidelity Design Optimization using Adaptive Sampling and Polynomial Chaos Kriging Model,” 58th AIAA/ASCE/AHS/ASC Structures, Structural Dynamics, and Materials Conference, Grapevine, TX, U.S.A., Jan. 9-13, 2017. (https://doi.org/10.2514/1.12466)

[13] Yeongmin Jo, Se Hwan Park, Duck-Joo Lee, and Seongim Choi, “Development of A Three-Dimensional Tightly Coupled Euler/Potential Flow Solver for Transonic Flow,” 30th Congress of the International Council of the Aeronautical Sciences, Daejeon, South Korea, Sep. 26-29, 2016.

[12] Yeongmin Jo, Se Hwan Park, Duck-Joo Lee, and Seongim Choi. "Development of An Efficient Three-Dimensional Tightly Coupled Euler/Potential Solver for Transonic Flow Analysis," 34th AIAA Applied Aerodynamics Conference, Washington, D.C., U.S.A., Jun. 13-17, 2016. (https://doi.org/10.2514/6.2016-3867)

[11] Yeongmin Jo, Seongim Choi, Lauren Zientarski, and James J. Joo. "Aerodynamic Characteristics and Shape Optimization of a Variable Camber Compliant Wing," 34th AIAA Applied Aerodynamics Conference, Washington, D.C., U.S.A., Jun. 13-17, 2016. (https://doi.org/10.2514/6.2016-3416)

[10] Jangho Park, Yeongmin Jo, Seulgi Yi, Jae-Young Choi, Pradeep Raj, and Seongim Choi. "Variable-Fidelity Multidisciplinary Design Optimization for Innovative Control Surface of Tailless Aircraft," 34th AIAA Applied Aerodynamics Conference, Washington, D.C., U.S.A., Jun. 13-17, 2016. (https://doi.org/10.2514/6.2016-4038)

[9] Jangho Park, Jae-Young Choi, Yeongmin Jo, and Seongim Choi. "Stability Derivative Computation of Tailless Aircraft using Variable-Fidelity Aerodynamic Analysis for Control Performance Analysis," 54th AIAA Aerospace Sciences Meeting, San Diego, CA, U.S.A., Jan. 4-8, 2016. (https://doi.org/10.2514/6.2016-2024)

[8] Yeongmin Jo, Jangho Park, Seongim Choi, and Duckjoo Lee. "Adaptive Variable-Fidelity Analysis and Design for A Tailless Aircraft with Innovative Control Effectors under Model-Form Uncertainty," 57th AIAA/ASCE/AHS/ASC Structures, Structural Dynamics, and Materials Conference, San Diego, CA, U.S.A., Jan. 4-8, 2016. (https://doi.org/10.2514/6.2016-0163)

[7] Jangho Park, Jaeyoung Choi, Christopher Ocheltree, Yeongmin Jo, and Seongim Choi, “Stability Derivative Computation of Tailless Aircraft using Variable-Fidelity Aerodynamic Analysis,” 33rd AIAA Applied Aerodynamics Conference, Dallas, TX. U.S.A., Jun. 22-26, 2015. (https://doi.org/10.2514/6.2016-2024)

[6] Yeongmin Jo, Jangho Park, Jaeyoung Choi, Christopher Ocheltree, Seongim Choi, and Duckjoo Lee, “Adaptive Variable-Fidelity Aerodynamic Analysis and Design for Tailless Aircraft under Model-Form Uncertainty,” 16th AIAA/ISSMO Multidisciplinary Analysis and Optimization Conference, Dallas, TX. U.S.A., Jun. 22-26, 2015. (https://doi.org/10.2514/6.2015-3235)

[5] Yeongmin Jo, Seongim Choi, and Duckjoo Lee, “Variable-Fidelity Design Using Kriging Surrogate Model with Fidelity Indicator,” 56th AIAA/ASCE/AHS/ASC Structures, Dynamics, and materials Conference, Kissimmee, FL. U.S.A., Jan. 5-9, 2015. (https://doi.org/10.2514/6.2015-1365)

[4] Yeongmin Jo, Seongim Choi, and Duckjoo Lee, “Variable-Fidelity Design Method Using Gradient-Enhanced Kriging Surrogate Model with Regression,” 14th AIAA Aviation Technology, Integration, and Operations Conference, Atlanta, GA. U.S.A., Jun. 16-20, 2014. (https://doi.org/10.2514/6.2014-2867)

[3] Yeongmin Jo, and Seongim Choi, “Variable-Fidelity Aerodynamic Design Using Gradient Enhanced Kriging Surrogate Model with Regression,” 52nd Aerospace Sciences Meeting, National Harbor, MD, U.S.A., Jan. 13-17. 2014. (https://doi.org/10.2514/6.2014-0900)

[2] Youngmin Jo, Hakjin Lee, and Seongim Choi, “Aerodynamic Design Optimization of Wing-Sails,” 31st AIAA Applied Aerodynamics Conference, San Diego, CA. U.S.A., Jun. 24-27. 2013. (ttps://doi.org/10.2514/6.2013-2524)

[1] Youngmin Jo, Seongim Choi, and Youngmin Park, “Development and Validation of Conceptual Design Framework for Mid-Size Turbo-Prop Transport,” 51st AIAA Aerospace Science Meeting including the New Horizons Forum and Aerospace Exposition, Grapevine, TX. U.S.A., Jan. 7-10. 2013. (https://doi.org/10.2514/6.2013-620)