Effects of Constant Turbulent Eddy Viscosity Assumption on Gradient-Based Design Optimization
C. S. Kim, C. Kim and O. H. Rho
40th AIAA Aerospace Sciences Meeting and Exhibit, , . (January 2002)
Dynamic Stall Control Using Aerodynamic Sensitivity Analysis
T. Ahn, H. Kim, C. Kim and O. Rho39th AIAA Aerospace Sciences Meeting and Exhibit, , . (January 2001)
Doi:10.2514/6.2001-255
Analysis of Rarefied Nozzle Flow by Generalized Hydrodynamic Equations
D. Chae, C. Kim, O. Rho and R.S. Myong39th AIAA Aerospace Sciences Meeting and Exhibit, , . (January 2001)
Doi:10.2514/6.2001-894
Aerodynamic Sensitivity Analysis for Turbulent Flow on Chimera Overlaid Grids
C. S. Kim, C. Kim, O. H. Rho39th AIAA Aerospace Sciences Meeting and Exhibit, , . (January 2001)
Doi:10.2514/6.2001-267
Aerodynamic Sensitivity Analysis for Turbulent Flow on Chimera Overlaid Grids
C. S. Kim, C. Kim and O. H. Rho
39th AIAA Aerospace Sciences Meeting and Exhibit, , . (January 2001)
Analysis of Rarefied Nozzle Flow by Generalized Hydrodynamic Equations
D. Chae, C. Kim, O. Rho and R.S. Myong
39th AIAA Aerospace Sciences Meeting and Exhibit, , . (January 2001)
Dynamic Stall Control Using Aerodynamic Sensitivity Analysis
T. Ahn, H. Kim, C. Kim and O. Rho
39th AIAA Aerospace Sciences Meeting and Exhibit, , . (January 2001)
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)
