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| ³í¹®¸í | ¹ßÇ¥ÇмúÁö¸í | Vol No | PP | ¹ßÇ࿬µµ |
| Lower-Upper Symmetric Gauss-Seidel Scheme Exhibiting Asymmetric Vortices over Slender Bodies | Journal of Spacecraft and Rockets | 33(5) | 750-752 | 1996 |
| Dual-point design of transonic airfoils using the hybrid inverse optimization method | Journal of Aircraft | 34(5) | 612-618 | 1997 |
| An Improvement of AUSM Schemes by Introducing the Pressure-based Weight Functions | Computers and Fluids | 27(3) | 311-346 | 1998 |
| Aerodynamic design of transonic wings using the target pressure optimization approach | Journal of Aircraft | 35(5) | 671-677 | 1998 |
| Numerical Simulation of the Flowfield Around Airfoil with Stationary or Oscillating Spoiler | Journal of Aircraft | 35(5) | 704-711 | 1998 |
| Multipoint Inverse Design Method for Transonic Wings | Journal of Aircraft | 36(6) | 941-947 | 1999 |
| Development of an Improved Gas-kinetic BGK scheme for Inviscid and Viscous Flows | Journal of Computational Physics | 158(1) | 1-27 | 2000 |
| Numerical Analysis of Hypersonic Shock-Shock Interaction using AUSMPW+ Scheme and Gas Reaction Model | KSAS International Journal | 1(1) | 21-28 | 2000 |
| Chimera °ÝÀÚ±â¹ýÀÇ º´·Ä󸮸¦ ÀÌ¿ëÇÑ 3´ÜÇü ·ÎÄÏÆ®ÀÇ ºñÁ¡¼ºÀ¯µ¿ ÇØ¼® | Çѱ¹Ç×°ø¿ìÁÖÇÐȸÁö | 28(1) | 10-19 | 2000 |
| Chimera °ÝÀÚ±â¹ýÀÇ º´·Ä󸮸¦ ÀÌ¿ëÇÑ ´Ù´Ü ·ÎÄÏÆ®ÀÇ Á¡¼ºÀ¯µ¿Çؼ® | Çѱ¹Ç×°ø¿ìÁÖÇÐȸÁö | 28(8) | 25-32 | 2000 |
| Parallel Computations of High-Lift Airfoil Flows Using Two-Equation Turbulence Models | AIAA Journal | 38(8) | 1360-1369 | 2000 |
| Sensitivity Analysis for the Navier-Stokes Equations with Two-Equation Turbulence Models | AIAA Journal | 39(5) | 838-845 | 2001 |
| Single and High-Lift Airfoil Design Optimization Using Aerodynamic Sensitivity Analysis | KSAS International Journal | 2(1) | 20-27 | 2001 |
| Numerical Analysis on Separation Dynamics of Strap-On Boosters in the Dense Atmosphere | KSAS International Journal | 2(2) | 1-18 | 2001 |
| Multigrid Algorithm for Computing Hypersonic, Chemically Reacting Flows | Journal of Spacecraft and Rockets | 38(6) | 865-874 | 2001 |
| Response Surface Method for Airfoil Design in Transonic Flow | Journal of Aircraft | 38(2) | 232-238 | 2001 |
| Inverse Design of Transonic Wings Using Wing Planform and Target Pressure Optimization | Journal of Aircraft | 38(4) | 644-652 | 2001 |
| Methods for the Accurate Computations of Hypersonic Flows, PART I : AUSMPW+ Scheme | Journal of Computational Physics | 174(1) | 38-80 | 2001 |
| Methods for the Accurate Computations of Hypersonic Flows, PART II : Shock-Aligned Grid Technique | Journal of Computational Physics | 174(1) | 81-119 | 2001 |
| AUSMPW+ ¼öÄ¡±â¹ý °³¹ß ¹× ºÐ¼® | Çѱ¹Ç×°ø¿ìÁÖÇÐȸÁö | 29(8) | 45-56 | 2001 |
| GH ¹æÁ¤½ÄÀ» ÀÌ¿ëÇÑ Èñ¹ÚÀ¯µ¿ÀÇ ¼öÄ¡Àû ÇØ¼® | Çѱ¹Ç×°ø¿ìÁÖÇÐȸÁö | 29(1) | 1-7 | 2001 |
| ´ÙÁß°ÝÀÚ±â¹ýÀ» ÀÌ¿ëÇÑ ±ØÃÊÀ½¼Ó À¯µ¿Àå °è»ê | Çѱ¹Ç×°ø¿ìÁÖÇÐȸÁö | 29(1) | 8-15 | 2001 |
| ¾ÐÃ༺ À¯µ¿ÀÇ ¼öÄ¡ÇØ¼® ¹× ¼öÄ¡ÇØ¹ý °³¹ß (BGK ±â¹ýÀÇ Àû¿ë) | Çѱ¹ÃßÁø°øÇÐȸÁö | 5(1) | 1-9 | 2001 |
| A Shock Stable Roe Scheme | Àü»êÀ¯Ã¼°øÇÐȸÁö | 6(4) | 43-53 | 2001 |
| ¹ÝÀÀ±âü ÇØ¼®À» À§ÇÑ À½¼Ó ¹× À½¼Ó¿¡ µû¸¥ ÇØÀÇ Á¤È®¼º ¿¬±¸ | Çѱ¹Ç×°ø¿ìÁÖÇÐȸÁö | 30(1) | 9-19 | 2002 |
| Ãæ°ÝÆÄ ¿µ¿ª¿¡¼ÀÇ AUSM °è¿ ¼öÄ¡±â¹ýÀÇ ´ÜÁ¶¼º¿¡ °üÇÑ ¿¬±¸ | Çѱ¹Ç×°ø¿ìÁÖÇÐȸÁö | 30(2) | 30-38 | 2002 |
| Ãæ°ÝÆÄ¿¡¼ÀÇ ¹°¼ºÄ¡ Áøµ¿Çö»ó¿¡ ´ëÇÑ ºÐ¼®°ú M-AUSMPW+ ¼öÄ¡±â¹ý °³¹ß | Çѱ¹Ç×°ø¿ìÁÖÇÐȸÁö | 30(2) | 21-29 | 2002 |
| AUSM°è¿ ¼öÄ¡±â¹ýÀÇ ¼öÄ¡Àû ºÒ¾ÈÁ¤¼º¿¡ ´ëÇÑ ºÐ¼® | Çѱ¹Ç×°ø¿ìÁÖÇÐȸÁö | 30(3) | 27-36 | 2002 |
| CFDS ±â¹ýÀ» ÀÌ¿ëÇÑ ³·ù À¯µ¿Àå ÇØ¼® | Çѱ¹Ç×°ø¿ìÁÖÇÐȸÁö | 30(3) | 105-114 | 2002 |
| Àú ·¹À̳îÁî¼ö À¯µ¿¿¡¼ Flapping-AirfoilÀÇ ¼öÄ¡Àû °ø·ÂƯ¼º ¿¬±¸ | Çѱ¹Ç×°ø¿ìÁÖÇÐȸÁö | 30(4) | 44-52 | 2002 |
| Numerical Analysis on Separation Dynamics of Strap-On Boosters in the Atmosphere | Journal of Spacecraft and Rockets | 39(3) | 439-446 | 2002 |
| Numerical Simulation of the Vortex-Fin Interaction over a Tangent-Ogive Cylinder | Aeronautical Journal | 106(1058) | 175-184 | 2002 |
| Multi-Block °ÝÀÚ±â¹ýÀ» ÀÌ¿ëÇÑ ÃʼÒÇü ºñÇàü ÁÖÀ§ °ø·ÂƯ¼º¿¬±¸ | Çѱ¹Ç×°ø¿ìÁÖÇÐȸÁö | 41(6) | 8-16 | 2003 |
| Flapping ¿îµ¿ÀÇ ÃÖÀû°ø·Â¼º´ÉÀ» À§ÇÑ ÀÍÇü¿¬±¸ | Àü»êÀ¯Ã¼°øÇÐȸÁö | 8(2) | 24-32 | 2003 |
| Cures for the Shock Instability: Development of Shock-Stable Roe Scheme | Journal of Computational Physics | 185(2) | 342-374 | 2003 |
| Feasibility Study of Constant Eddy-Viscosity Assumption in Gradient-Based Design Optimization | Journal of Aircraft | 40(6) | 1168-1176 | 2003 |
| Dynamic Stall Control Based On an Optimal Approach | Journal of Aircraft | 41(5) | 1106-1116 | 2004 |























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