Showing results 1 to 5 of 5
An analysis of screech tone noise and its mode change of an axisymmetric supersonic jet using an optimized compact scheme Lee, I.C.; Kim, J.W.; Lee, Duck-Joo, 10th AIAA/CEAS Aeroacoustics Conference, v.2, pp.1712 - 1719, American Institute of Aeronautics and Astronautics, 2004-05-10 |
Comparative Study of Numerical Schemes of TVD3, UNO3-ACM and Optimized Compact Scheme Lee, Duck-Joo; Hwang, C.J.; Ko, D.K.; Kim, J.W., ICASE, no.3300, pp.47 - 57, NASA, 1994-10 |
Hovering rotor computation including aero-elastic effects with an overlapped grid Navier-Stokes solver Kim, J.W.; Park, S.H.; Ko, J.H.; Park, I.-J.; Jung, S.N.; Yu, N.H.; Kim, E; et al, 26th AIAA Applied Aerodynamics Conference, AIAA, 2008-08-18 |
Numerical Study on Radiation of Multiple Pure Tone Noise From and Aircraft Engine Inlet Shim, I.B.; Kim, J.W.; Lee, Duck-Joo, 5th AIAA/CEAS Aeroacoustics, 1999-01 |
Study on noise characteristics of open cavity with cross-correlation analysis Lee, Duck-Joo; Heo, D.N.; Kim, J.W., The Fifth JSME-KSME Fluids Engineering Conference, pp.2003 - 3104, 2002 |
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