Browse "Dept. of Aerospace Engineering(항공우주공학과)" by Author Kwon, Jang-Hyuk
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| 2차 upwind TVD 기법을 위한 개선된 다단계 시간 전진 기법 = An improved multistage time stepping for 2nd order upwind TVD schemeslink 박태상; Park, Tae-Sang; et al, 한국과학기술원, 1998 |
| 2차원 Euler/N-S 방정식에 대한 민감도 해석 기법의 성능 비교 연구 = A comparative study of the sensitivity analysis of two dimensional Euler/N-S equationslink 임동균; Im, Dong-Kyun; et al, 한국과학기술원, 2007 |
| 3-D Wing Shape Optimization Based on Grid Computing Kim, D.; Kim, S.; Kwon, Jang-Hyuk; Sung, C.-H.; Cho, K.W., Second China-Japan-Korea Joint Symposium on Optimization of Structural and Mechanical Systems, pp.737 - 742, 2002 |
| 3-D wing simulation with design optimization on grid computing environment Cho, Kumwon; Sung, Chunho; Lee, Sangsan; Kim, Dehee; Kwon, Jang-Hyuk, Scientific and Organizing Committee, pp.0 - 0, 2003-05 |
| A high order scheme using hybrid methodology Kwon, Jang-Hyuk, KAIST-Kyushu Uni Mechanical and Aerospace Engineering, pp.0 - 0, 2004-09 |
| A high-order accurate hybrid scheme using a central flux scheme and a WENO scheme for compressible flowfield analysis Kim, D; Kwon, Jang-Hyuk, JOURNAL OF COMPUTATIONAL PHYSICS, v.210, no.2, pp.554 - 583, 2005-12 |
| A hybrid time-stepping method of local preconditioning on high aspect ratio grids Lee, Jae-Eun; Kim, Yoon-Sik; Kwon, Jang-Hyuk, JOURNAL OF MECHANICAL SCIENCE AND TECHNOLOGY, v.25, no.3, pp.741 - 747, 2011-03 |
| A low dissipative and dispersive scheme with a high order WENO dissipation for unsteady flow analyses Kim, Dehee; Kwon, Jang-Hyuk, AIAA fluid dynamics conference, pp.2705, AIAA, 2004-06 |
| A new discretization method of governing equations for high order accuracy Kim, Dehee; Kwon, Jang-Hyuk, The Global CFD Committee, v.3, pp.429 - 434, 2004-07 |
| A New Efficient 2-D Chimera Methodology: CHOG2D Cho, K.W.; Kwon, Jang-Hyuk, Symposium on Overset Composite Grid & Solution Technology, pp.101 - 120, 1998 |
| A Non-Iterative Method for the Elliptic Generation of Three-Dimensional Grids by Using the Boundary Element Method Jeong, H. K; Kwon, Jang-Hyuk, Int. Conf. on Numerical Grid Generation in Computational Field Simulations, pp.127 - 136, 1996-04 |
| A Preconditioned HLLE Method for Flows at All Mach Numbers Park, S.H.; Kwon, Jang-Hyuk, AIAA Fluid Dynamics Conference and Exhibit, pp.2709 - 2709, AIAA, 2004-06 |
| 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 |
| A Study on the Aerodynamic Shape Design Optimization of the Airfoil with the PARSEC Function Lee, Jaehun; Kwon, Jang-Hyuk, 7th World Congress on Structural and Multidisciplinary Optimization, International Society for Structural and Multidisciplinary Optimization, 2007-05 |
| A Study on the Far-Field Boundary Condition Effects of CFD/Time-Marching-Free-Wake Coupled Method Wie, Seong-Yong; Im, Dong-Kyun; Kwon, Jang-Hyuk; Lee, Duck-Joo, AHS Specialists' Conference, 2007-10 |
| A Three-Dimensional Grid Generation Method for Nearly Orthogonal Grid Near Boundaries Using the Covariant Laplace Equations Kwon, Jang-Hyuk, COMPUTATIONAL FLUID DYNAMICS JOURNAL, v.6, no.1, pp.111 - 128, 1997-01 |
| Accurate aerodynamic sensitivity analysis using adjoint equations Sung, CH; Kwon, Jang-Hyuk, AIAA JOURNAL, v.38, no.2, pp.243 - 250, 2000-02 |
| Adjoint 방법을 이용한 효율적인 공력 최적 설계 = An efficient aerodynamic design optimization using the adjoint methodlink 성춘호; Sung, Chun-Ho; et al, 한국과학기술원, 2000 |
| Adjoint 방정식을 이용한 날개 형상 최적설계에 대한 연구 = A study on wing optimization design using adjoint equationlink 배효길; Bae, Hyo-Gil; et al, 한국과학기술원, 1999 |
| Aerodynamic Analysis of Rotor Blades using Overset Grid by means of Parallel Computation Im, D.K.; Wie, S.Y.; Kim, E.; Kwon, Jang-Hyuk; Lee, Duck-Joo, 20th International Series of Meetings on Parallel Computational Fluid Dynamics, CFD 2008, pp.101 - 110, 2008-05-19 |
| Aerodynamic design optimization using the Navier-Stokes and adjoint equations Sung, C.-h.; Kwon, Jang-Hyuk, AIAA Aerospace Sciences Meeting and Exhibit, AIAA, 2001-01 |
| Aeroelastic Analysis of Three-dimensional Wing Using a Parallel Euler Solver Kwon, H. J; Park, S.H; Kim, Y.S; Kim, J.Y; Lee, In; Kwon, Jang-Hyuk, KSAS 1st International Sessions in 2003 KSAS Fall Conference, The Korean Society for Aeronautical and Space Sciences, 2003-11 |
| An Efficient Strategy for Reliability-Based Multidisciplinary Design Optimization Ahn, Joongki; Kwon, Jang-Hyuk, 2004 KSAS-JSASS Joint Symposium on Aerospace Engineering, pp.294 - 301, 2004 |
| An efficient strategy for reliability-based multidisciplinary design optimization using BLISS Ahn, J; Kwon, Jang-Hyuk, STRUCTURAL AND MULTIDISCIPLINARY OPTIMIZATION, v.31, no.5, pp.363 - 372, 2006-05 |
| An improved HLLE method for hypersonic viscous flows Park, S.H.; Kwon, Jang-Hyuk, AIAA CFD Conference, pp.733 - 743, AIAA, 2001-06 |
| An Improved Multistage Time Stepping for 2nd Order Upwind TVD Schemes for the Navier-Stokes Equation Kwon, Jang-Hyuk, Asian Computational Fluid Dynamics Conference, pp.145 - 150, 1996 |
| An improved multistage time stepping for second-order upwind TVD schemes Park, TS; Kwon, Jang-Hyuk, COMPUTERS FLUIDS, v.25, no.7, pp.629 - 645, 1996-09 |
| An Upwind Finite Element Method Using Optimal Weighting Functions for Solving Compressible Euler Equations Kwon, Jang-Hyuk, COMPUTATIONAL FLUID DYNAMICS JOURNAL, v.4, no.3, pp.293 - 301, 1995-10 |
| Analysis of Implicit Preconditioners for Multigrid Calculations on the High Reynolds Number Turbulent Flows Kim, Yoonsik; Kwon, Jang-Hyuk, CFD JOURNAL, v.12, no.4, pp.606 - 613, 2004-01 |
| Application of Multistage Time Stepping Method for 2nd Order Upwind TVD Schemes Oh, B.S.; Kwon, Jang-Hyuk, Flow Modeling and Turbulence Measurements, pp.141 - 150, 1998 |
| Comparative Study of k-w Turbulence Models for Transonic Separated Flows Park, S.H.; Kwon, Jang-Hyuk, Asian CFD, pp.260 - 267, 2003 |
| Comparisons of steady and unsteady methods for pitch-damping predictions Park, Soo Hyung; Kwon, Jang-Hyuk, the 21st AIAA Applied Aerodynamics Conference, pp.0 - 0, AIAA, 2003-06 |
| Computation of roll moment for projectile with wraparound fins using Euler equation Paek, SK; Park, TS; Bae, JS; Lee, In; Kwon, Jang-Hyuk, JOURNAL OF SPACECRAFT AND ROCKETS, v.36, no.1, pp.53 - 58, 1999 |
| Computational Aerodynamic Characteristics of Wing with End-Plate for WIG Kwon, Jang-Hyuk, ParCFD, pp.47 - 48, 2006-05 |
| Convergence Acceleration of k-w Turbulence Equations With Multigrid Park, S.H.; Sung, C.H.; Kwon, Jang-Hyuk, Computational technologies for Fluid/Thermal/Structural/Chemical Systems with Industrial Applications (2002 ASME Prssure Vessels and Piping Conference), v.448, no.1, pp.35 - 44, 2002-08-05 |
| Correction of Ground Effect for Whirl Tower Test using CFD/Freewake Coupling Method Jang, Ji-Sung; Wie, Seong-Yong; Lee, Duck-Joo; Kwon, Jang-Hyuk; Song, Keun-Woong; Jeong, Ki-Hoon, 1st Asian/Australian rotorcraft forum and Exhibition, ARF2012 Executive Committee, 2012-02-14 |
| Covariant 라플라스 방정식을 이용한 경계에 근사적으로 직교하는 삼차원 격자형성방법 개발 = Development of three-dimensional grid generation method for nearly orthogonal grids near boundaries using the covariant laplace equationslink 정희권; Jeong, Hee-Kwon; et al, 한국과학기술원, 1997 |
| 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 optimization using CFD Kwon, Jang-Hyuk, KSEA-KOFST-KUSCO, pp.0 - 0, 2004-08 |
| Development of a fully systemized chimera methodology for steady/unsteady problems Cho, KW; Kwon, Jang-Hyuk; Lee, S, JOURNAL OF AIRCRAFT, v.36, no.6, pp.973 - 980, 1999 |
| Drag Prediction of DLR-F6 Using the Turbulent Navier-Stokes Calculations with Multigrid Kim, Y.; Park, S.H.; Kwon, Jang-Hyuk, AIAA aerospace Sciences Meeting and Exhibit, v.42, AIAA, 2004-01 |
| Drag prediction of DLR-F6 using the turbulent navier-stokes calculations with multigrid Kim, Y.; Park, S.H.; Kwon, Jang-Hyuk; Sung, C.-H., 42nd AIAA Aerospace Sciences Meeting and Exhibit, pp.335 - 345, American Institute of Aeronautics and Astronautics, 2004-01-05 |
| Effect of afterbody configuration on damping coefficients for axisymmetric projectiles Park, SH; Kwon, Jang-Hyuk, JOURNAL OF SPACECRAFT AND ROCKETS, v.41, no.6, pp.1065 - 1068, 2004-11 |
| Efficient aerodynamic design method using a tightly coupled algorithm Sung, CH; Kwon, Jang-Hyuk, AIAA JOURNAL, v.40, no.9, pp.1839 - 1845, 2002-09 |
| Efficient Aeroelastic Analysis Method Including Inverse Design for Body Effects Lee, Seung-Jun; Im, Dong-Kyun; Kang, Myung-Koo; Lee, In; Kwon, Jang-Hyuk, JOURNAL OF AIRCRAFT, v.46, no.6, pp.2164 - 2169, 2009-11 |
| Efficient global design optimization incorporating expected functions estimation criteria = 기대함수 평가 기준을 적용한 효율적인 전역 최적설계기법 연구link Lee, Chang-Hyuck; 이창혁; et al, 한국과학기술원, 2012 |
| Efficient global optimization for S-duct diffuser shape design Bae, Hyo-Gil; Park, Soo-Hyung; Kwon, Jang-Hyuk, PROCEEDINGS OF THE INSTITUTION OF MECHANICAL ENGINEERS PART G-JOURNAL OF AEROSPACE ENGINEERING, v.227, no.9, pp.1516 - 1532, 2013-09 |
| Efficient global optimization incorporating feasibility criterion for the design of a supersonic inlet Lee, Chang-Hyuck; Ahn, J-K; Bae, Hyo-Gil; Kwon, Jang-Hyuk, PROCEEDINGS OF THE INSTITUTION OF MECHANICAL ENGINEERS PART G-JOURNAL OF AEROSPACE ENGINEERING, v.226, no.G11, pp.1362 - 1372, 2012-11 |
| Efforts in developing design and simulation tools for MEMS: DS/MEMS and CA/MEMS Youn, Sung-Kie; Kwak, Byung Man; Kwon, Jang-Hyuk; Chang, Su-Young; Huh, Jae S.; Kim, Eugene, Symposium on Design/Test/Integration and Packaging of MEMS/MOEMS, 2002, v.4755, pp.275 - 284, 2002-01 |
| EGO method for diffusing S-duct Shape Design Bae, Hyo-Gil; Park, Soo-Hyung; Kwon, Jang-Hyuk, Seventh International Conference on Computational Fluid Dynamics, Computational Fluid Dynamics, 2012-07-09 |
| Evaluation of Longitudinal Stability Characteristics Based on Irodovs Criteria for Wing-In-Ground Effect Shin, Seung-Yun; Whang, Kyung-Hyun; Kim, Kyun-Seok; Kwon, Jang-Hyuk, TRANSACTIONS OF THE JAPAN SOCIETY FOR AERONAUTICAL AND SPACE SCIENCES, v.53, no.182, pp.237 - 242, 2011-02 |
| Far-Field Boundary Condition Effects of CFD and Free-Wake Coupling Analysis for Helicopter Rotor Wie, SY; Lee, JH; Kwon, Jang-Hyuk; Lee, Duck-Joo, JOURNAL OF FLUIDS ENGINEERING-TRANSACTIONS OF THE ASME, v.132, no.8, 2010-08 |
| Flow Calculations in JPL Nozzle Using the Solution-Adaptive Grid Generation Park, T. S; Kwon, Jang-Hyuk, Pan-Pacific Conference, v.11, pp.103 - 106, 1993-11 |
| Flow calculations on GRID environment Kim, D.; Kim, Y.; Park, S.H.; Kwon, Jang-Hyuk, The Asian CFD Society, pp.0 - 0, 2003-10-01 |
| Flow Simulation for DLR F6 wing-body configuration with and without FX2B Im, D.K.; Kwon, Jang-Hyuk, HPC Asia Conference, 2007 |
| Helicopter rotor noise in the merged tip-vortex and blade interaction condition Wie, Seong-Yong; Im, Dong-Kyun; Kwon, Jang-Hyuk; Lee, Duck-Joo; Chung, K. H.; Kim, S. B., INTERNATIONAL JOURNAL OF AEROACOUSTICS, v.10, pp.427 - 442, 2011 |
| Hovering rotor computation including aero-elastic effects with an overlapped grid Navier-Stokes solver Kim, J.W.; Park, S.H.; Ko, J.H.; Park, I.-J.; Jung, S.N.; Yu, N.H.; Kim, E; et al, 26th AIAA Applied Aerodynamics Conference, AIAA, 2008-08-18 |
| Implementation of k-omega turbulence models in an implicit multigrid method Park, SH; Kwon, Jang-Hyuk, AIAA JOURNAL, v.42, no.7, pp.1348 - 1357, 2004-07 |
| Implicit preconditioners for the 2-D multigrid Navier-Stokes solvers Kim, Yoonsik; Kwon, Jang-Hyuk, the 16th AIAA Computational Fluid Dynamics Conference, pp.0, AIAA, 2003-06 |
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