| 1 | Sound Generation from Evolution of Elliptic Vortex Ring and a Vortex Ring Intergration with a Rigid Sphere Ryu, K. W.; Lee, Duck-Joo, 34th AIAA Aerosp ace Science Meeting, AIAA, 1996-01 |
| 2 | Comparison of High-Order ENO Schemes for Compressible Flows Ko, D. K.; Lee, Duck-Joo, Asian CFD Conference Japan Serial 2, pp.69 - 74, 1996-09 |
| 3 | Predictions of airloads and wake geometry for slowly starting rotor blades in hovering flight by using time marching free vortex blob method Lee, Duck-Joo; Na, Seon Uk, Proceedings of the 1996 52nd Annual Forum. Part 1 (of 3), v.1, pp.532 - 539, 1996-06-04 |
| 4 | Sound Generation Due to a Spinning Vortex Pair near the Flat and Curved Wall Koo, S. O.; Ryu, K. W.; Lee, Duck-Joo, 2nd AIAA/CEAS Aero Acoustic Conference, AIAA, 1996-05 |
| 5 | Optimized Compact Finite Difference Schemes for Solving Wave Equations Kim, J. W.; Lee, Duck-Joo, 16th AIAA Aeroacoustic Conference, AIAA, 1996-06 |
| 6 | Optimized High-Order Compact Schemes for Linear and Nonlinear Wave Generation and Propagation Kim, J. W.; Lee, Duck-Joo, pp.905 - 912, 1996-07 |
| 7 | Implementation of Boundary Conditions for the High Order Optimized Compact Schemes Kim, J. W; Lee, Duck-Joo, 2nd AIAA/CEAS Aero Acoustic Conference, AIAA, 1996 |
| 8 | Third Order Uniformly Non-Oscillatory Schemes with Modified ACM Technique for Linear Wave and Euler Equcation Lee, Duck-Joo, AIAA, 1996 |
| 9 | High-Resolution, Nonoscillatory Schemes with Modified ACM Method for Compressible Flow Ko, D. K.; Lee, Duck-Joo, AIAA/CEAS Aeroacoustics Conference, 1996-05 |
| 10 | Diffraction by Thin-Walled Shapes of Revolution with Compliant Boundary Conditions by Using the Direct Boundary Element Method Ih, K.D.; Lee, Duck-Joo, AIAA Aerospace Sciences Meeting, AIAA, 1996-01 |
