Showing results 1 to 21 of 21
A Preliminary Study for the Design of Open Rotor Using Harmonic Balance Method Jang, Ji-Sung; Choi, Seongim; Kwon, Hyung-Il; Im, Dong-Kyun; Lee, Duck-Joo; Kwon, Jang-Hyuk, 50th AIAA Aerospace Sciences Meeting including the New Horizons Forum and Aerospace Exposition, 50th AIAA Aerospace Science Meeting, 2012-01-12 |
A preliminary study of open rotor design using a harmonic balance method Kwon, Hyungil; Choi, Seongim; Jang, Jisung; Im, Dongkyun; Lee, Duck-Joo; Kwon, Jang-Hyuk, 1st Asian/Australian rotorcraft forum and exhibition, ARF2012 Executive Committee, 2012-02-14 |
Adaptive Variable-Fidelity Analysis and Design Using Dynamic Fidelity Indicators Jo, Yeongmin; Yi, Seulgi; Choi, Seongim; Lee, Duck-Joo; Choi, Dong-Zin, AIAA JOURNAL, v.54, no.11, pp.3564 - 3579, 2016-11 |
Aerodynamic design optimization of control surfaces for a tailless aircraft at high angles of attack Jo, Yeongmin; Park, Jangho; Choi, Seongim; Lee, Duck-Joo, 57th AIAA/ASCE/AHS/ASC Structures, Structural Dynamics, and Materials Conference, 2016, American Institute of Aeronautics and Astronautics Inc, AIAA, 2016-01 |
An Efficient Fluid-Structure Interaction Analysis based on Time-Spectral Approaches Yi, Seulgi; Choi, Seongim; Im, Dongkyun; Lee, Duck-Joo, 56th AIAA/ASCE/AHS/ASC structures, Structural Dynamics, and Materials Conference, AIAA SciTech, 2015-01-06 |
Design of a Low-Noise Open Rotor Using an Implicit Harmonic Balance Method Kwon, Hyung Il; Yi, Seulgi; Choi, Seongim; Lee, Duck-Joo; Kwon, Jang-Hyuk; Im, Dong-Kyun, 51th AIAA aerospace science meeting, pp.1 - 17, American Institute of Aeronautics and Astronautics(AIAA), 2013-01-10 |
Design of an Optimal Route Structure Using Heuristics-Based Stochastic Schedulers Choi, Seongim, IEEE/AIAA 29thDigital Avionics Systems Conference (DASC), 2010-10-06 |
Development of A Three-Dimensional Tightly Coupled Euler/Potential Flow Solver For Transonic Flow Jo, Yeong Min; Park, Se Hwan; Lee, Duck Joo; Choi, Seongim, 30th Congress of the International Council of the Aeronautical Sciences, International Council of the Aeronautical Sciences, 2016-09-29 |
Development of an efficient three-dimensional tightly coupled Euler/panel solver for transonic flow analysis Jo, Yeongmin; Lee, Duck-Joo; Choi, Seongim, 34th AIAA Applied Aerodynamics Conference, 2016, American Institute of Aeronautics and Astronautics Inc, AIAA, 2016-06 |
Development of An Efficient Tightly Coupled Euler/Panel Solver for Transonic Flow Analysis Jo, Yeong Min; Park, Se Hwan; Lee, Duck Joo; Choi, Seongim, AIAA Aviation 2016, AIAA, 2016-06-14 |
Efficient design optimization of flexible CROR blade for low-level noise Yi, Seulgi; Choi, Seongim; Im, Dongkyun; Lee, Duck-Joo, 34th AIAA Applied Aerodynamics Conference, 2016, American Institute of Aeronautics and Astronautics Inc, AIAA, 2016-06 |
Node-based spacecraft radiator design optimization Kim, Huikyung; Choi, Seongim; Park, Seung-O; Lee, Kyun Ho, ADVANCES IN SPACE RESEARCH, v.55, no.5, pp.1445 - 1469, 2015-03 |
Noise Characteristics of Contra-Rotating Open Rotor with Time-Spectral CFD and Aeroacoustics Analysis Yi, Seulgi; Kwon, Hyungil; Im, Dong Kyun; Choi, Seongim; Lee, Duck Joo, AIAA SciTech 2016, AMER INST AERONAUT ASTRONAUT, 2016-01-06 |
Parameter Study of Low Noise CROR System Yi, Seulgi; Kwon, Hyung Il; Choi, Seongim; Park, Min Jun; Lee, Duck Joo, AIAA Aviation 2016, AIAA, 2016-06-15 |
Rotor Flow Analysis using an Implicit Harmonic Balance Method Im. D; Choi, Seongim; Kwon, H; Park. S. H; Kwon, Jang-Hyuk, World Academy of Sicience Engineering and Technology 79 2011, pp.151 - 157, International Conference on Computational Fluid Dynamics, 2011-07 |
Rotor flow analysis using animplicit harmonic balance method Im, D.; Choi, Seongim; Kwon, H.; Park, S.H.; Kwon, Jang-Hyuk, World Academy of Science, Engineering and Technology, v.79, no.0, pp.151 - 157, 2011-07 |
Surrogate model based design optimization of multiple wing sails considering flow interaction effect Lee,Hakjin; Jo, Youngmin; Lee, Duck-Joo; Choi, Seongim, OCEAN ENGINEERING, v.121, pp.422 - 436, 2016-07 |
Surrogate-Based Robust Optimization and Design to Unsteady Low-Noise Open Rotors Kwon, Hyungil; Choi, Seongim; Kwon, Jang-Hyuk; Lee, Duckjoo, JOURNAL OF AIRCRAFT, v.53, no.5, pp.1448 - 1467, 2016-10 |
Unsteady rotor flow analysis using a diagonally implicit harmonic balance method and an overset mesh topology Im, Dong-Kyun; Choi, Seongim; Kwon, Jang-Hyuk, INTERNATIONAL JOURNAL OF COMPUTATIONAL FLUID DYNAMICS, v.29, no.1, pp.82 - 99, 2015-01 |
Variable-fidelity aerodynamic design using gradient-enhanced kriging surrogate model with regression Jo, Young Min; Choi, Seongim; Lee, Duck-Joo, AIAA Aviaation 2014, AIAA, 2014-06-18 |
Variable-Fidelity Design Using Kriging Surrogate Model with Fidelity Indicator Jo, Young Min; Choi, Seongim; Yi, Seulgi; Lee, Duck-Joo, 56th AIAA/ASCE/AHS/ASC structures, Structural Dynamics, and Materials Conference, AIAA SciTech, 2015-01-07 |
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