International Conference
[33] KyeongTae Yoo, and Yeongmin Jo, "Mission-Weighted Infill Sampling and Dynamic Fidelity Indicator for Efficient Aerodynamic Surrogates," AIAA SciTech 2027 Forum, Orlando, FL. U.S.A., Jan. 11-15. 2027. (Abstract submitted)
[32] Yoojin Chang, Dohyun Kim, Geonwoo Kim, Minsoo Park, and Yeongmin Jo, "Downwash Outwash Mitigation in UAM Vertiports Using Ground Surface Patterning," AIAA SciTech 2027 Forum, Orlando, FL. U.S.A., Jan. 11-15. 2027. (Abstract submitted)
[31] Junyoung Lee, and Yeongmin Jo, "Numerical Investigation of Slot Effects on the Aerodynamic and Aeroacoustic Characteristics of an SUAS Propeller," AIAA SciTech 2027 Forum, Orlando, FL. U.S.A., Jan. 11-15. 2027. (Abstract submitted)
[30] KyeongTae Yoo, and Yeongmin Jo, "Mission-Weighted Infill Sampling and Dynamic Fidelity Indicator for Efficient Aerodynamic Surrogates," APISAT 2026, Sapporo, Japan, Oct. 27-29. 2026. (Abstract accepted)
[29] Dogyun Kim, Sanghoon Jeong, and Yeongmin Jo, "Analysis of Interactional Aerodynamics and Acoustics between Rotor and Wing of a Tilt-Rotor Aircraft in Forward Flight," 52nd European Rotorcraft Forum, Amsterdam, Netherlands, Sep. 1-4. 2026. (Abstract accepted)
[28] Yoojin Chang, Dohyun Kim, Geonwoo Kim, Minsoo Park, and Yeongmin Jo, "CFD Investigation of Rotor Downwash–Outwash Characteristics over Patterned Ground Surfaces," 52nd European Rotorcraft Forum, Amsterdam, Netherlands, Sep. 1-4. 2026. (Abstract accepted)
[27] Seok-Jung Oh, Hyeok-Jin Son, Jae-Sang Park, Seokhyeon Shin, and Yeongmin Jo, "Performance and Vibration Analyses of a Quad Tiltrotor eVTOL Aircraft Considering Aerodynamic Interference Effects," 52nd European Rotorcraft Forum, Amsterdam, Netherlands, Sep. 1-4. 2026. (Abstract accepted)
[26] Seokhyeon Shin, Yeongmin Jo, and Joong-Kwan Kim, "Comparative Analysis of Subjective Annoyance between sUAS and Helicopter Noise: A Study on the Korean Public Response," INTER-NOISE 2026, Adelaide, Australia, Aug. 9-12. 2026. (Abstract accepted)
[25] Seokhyeon Shin, Yeongmin Jo, and Joong-Kwan Kim, "Blade Number Effects in sUAS Rotor Noise Assessed Using Psychoacoustic Metrics and an Online Listening Test," Quiet Drones 2026, Delft, Netherlands, Jun. 29-Jul. 1. 2026. (Abstract accepted)
[24] Yoojin Chang, Dohyun Kim, and Yeongmin Jo, "A Study on the Effects of Multi Rotor DWOW on the Human Body Using CFD," The 18th Asian Congress of Fluid Mechanics, Seoul, South Korea, Sep. 10-13. 2025.
[23] Seokhyeon Shin, Yeongmin Jo, and Seong-Yong Wie, "Psychoacoustic Analysis of Multiple UAM on an Urban Area," INTER-NOISE 2025, São Paulo, Brazil, Aug. 24-27. 2025.(https://doi.org/10.3397/in_2025_1077003)
[22] Yoojin Chang, Dohyun Kim, and Yeongmin Jo, "CFD Simulation of Multi Rotor-Induced DWOW and Its Effects on Human," The Seventh International Conference on Artificial Intelligence, Soft Computing, Machine Learning and Optimization in Civil, Structural and Environmental Engineering, Cagliari, Italy, Aug. 27-29. 2025. (https://doi.org/10.4203/ccc.10.9.6)
[21] Yeongmin Jo, "Development of An Environmental Noise Prediction Code for Rotorcrafts based on Flyover-Noise Measurements," Quiet Drones 2024, Manchester, United Kingdom, Sep. 8-11. 2024.
[20] Heegoo Lee, and Yeongmin Jo, "Analysis of Aerodynamic Interactions between An eVTOL Vehicle and Building," AJKFED 2023, Osaka, Japan, Jul. 9-13. 2023.
[19] Hyeonin Cho, Tae-Hwan Cho, Wanho Jeon, and Yeongmin Jo, "Development of A Community Noise Prediction Code for e-VTOL Vehicles," AIAA AVIATION 2023 Forum, San Diego, CA. U.S.A., Jun. 12-16. 2023. (https://doi.org/10.2514/6.2023-3360)
[18] Yeongmin Jo, "Aeroacoustic Analysis of eVTOL Rotors Considering Tonal and Broadband Noise Sources," 13th ACFD 2022, Jeju, South Korea, Oct. 16-19. 2022.
[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/Australian 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.
[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 Duck-Joo 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/10.2514/6.2015-3387)
[6] Yeongmin Jo, Jangho Park, Jaeyoung Choi, Christopher Ocheltree, Seongim Choi, and Duck-Joo 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 Duck-Joo 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 Duck-Joo 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] Yeongmin 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. (https://doi.org/10.2514/6.2013-2524)
[1] Yeongmin 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)