새로운 다차원 고차 내삽기법 개발
김규홍, 이정일, 김종암, 노오현춘계 한국항공우주학회, , . (April 2000)
병렬화된 Chimera 격자 기법을 이용한 3단형 로켓의 점성유동 해석
김성환, 김종암, 노오현춘계 한국항공우주학회, , . (April 2000)
Study of Accuracy Enhancement in Computational Fluid Dynamics
Kim, K. H., Lee, J. S., Kim, C. A., and Rho, O. HThe First Congress on Fluid Engineering, , . (March 2000)
Flow Control Using Unsteady Aerodynamic Sensitivity Analysis
H. J. Kim, C. Kim and O. H. Rho
38th AIAA Aerospace Sciences Meeting and Exhibit, , . (January 2000)
Doi:10.2514/6.2000-515
Aerodynamic Optimization of Supersonic Wing-Nacelle Configuration Using an Adjoint Method with the Unstructured-Grid Approach
H. J. Kim, C. Kim and O. H. Rho38th AIAA Aerospace Sciences Meeting and Exhibit, , . (January 2000)
A New Multi-Dimensional Interpolation Scheme for the Analysis of Compressible Flow
Kim K. H., Kim, C. A., and Rho O. H.AIAA Fluid 2000 Conference, , . (January 2000)
Application of Multigrid Method to Hypersonic Reacting Flows
Kim, S. S., Kim, C. A., and Rho, O. H.AIAA Fluid 2000 Conference, , . (January 2000)
Application of Multigrid Method to Hypersonic Reacting Flows
Kim, S. S., Kim, C. A. and Rho, O. H.
AIAA Fluid 2000 Conference, , . (January 2000)
A New Multi-Dimensional Interpolation Scheme for the Analysis of Compressible Flow
Kim K. H., Kim, C. A. and Rho O. H.
AIAA Fluid 2000 Conference, , . (January 2000)
Aerodynamic Optimization of Supersonic Wing-Nacelle Configuration Using an Adjoint Method with the Unstructured-Grid Approach
H. J. Kim, C. Kim and O. H. Rho
38th AIAA Aerospace Sciences Meeting and Exhibit, , . (January 2000)
