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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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