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| NO | Title, Author(s) (Publication Title, Volume Issue, Page, Issue Date) |
|---|---|
| Calculation of Vortex-Airfoil-Interaction by Using Vortex-In-Cell Method Chae, K. S.; Lee, Duck-Joo, The 27th Aircraft Symposium, pp.574 - 577, 1989-10 | |
| Effect of Phase Interference on Rotor Thickness Noise Park, S. C.; Lee, Duck-Joo, KSASS-Autumn, pp.195 - 202, 1989-10 | |
| Acoustic Measurements on Aerofoils Moving in a Circle at High Speed Wright, S. E.; Crosby, W.; Lee, Duck-Joo, AIAA 8th Aeroacoustics Conference, AIAA, 1983-04 | |
| Interaction of a Turbulent Vortex with a Lifting Surface Lee, Duck-Joo; Roberts, L., AIAA 23rd Aerospace Science Meeting, AIAA, 1985 | |
| Applications of Fast Vortex Method for the Interaction between Vortex and Wedge Corners Kim, Y. N.; Lee, Duck-Joo, KSASS-Autumn, pp.7 - 14, 1988-10 | |
| Impulsive Acoustic Wave Generation due to Turbulent Vortex and Lifting Surface Interaction Lee, Duck-Joo, KSASS-Spring, pp.27 - 32, 1988-05 | |
| Distortion of the Vortex Core during Blade/Vortex Interaction Lee, Duck-Joo; Smith, C. A., AIAA 19th Fluid Dynamics, Plasma Dynamics and Lasers Conference, AIAA, 1987-06 | |
| Prediction of Sources Moving at High Speed as Applied to Helicopter Noise Lee, Duck-Joo; Wright, S. E., AIAA 22nd Aerospace Science Meeting, AIAA, 1984-01 | |
| Surface Pressure Fluctuations due to Impinging Vortical Flows upon an Airfoil Lee, Duck-Joo, 1st National Fluid Dynamics Congress, pp.303 - 310, 1988-07 |