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Results 1-10 of 14 (Search time: 0.005 seconds).

NO Title, Author(s) (Publication Title, Volume Issue, Page, Issue Date)
1
Tip-vortex instability during the transition from hover to forward flight

Chung, K. H.; Hwang, C.; Yim, J. B.; Lee, Duck-Joo, Americal helicopter society, 2005-06

2
A prediction of transient behaviour using various vortex ring modelling

Yim, J. B.; Chung, K. H.; Lee, Duck-Joo, ICVFM 2005, pp.0 - 0, ICVFM, 2005-11

3
Investigation of parallel blade vortex interaction with split tip vortices

Cho, C. H.; Hwang, C.; Lee, Duck-Joo, 3rd International Conference on Vortex Flows and Vortex Models (ICVFM2005), pp.0 - 0, 2005-11-01

4
CAA(Computational Aeroacoustics) : Fundamental and its applications

Lee, Duck-Joo; Lee, I. C.; Cho, C. H., Korean-American Scientists and Engineers Association, 2005-08

5
Fan design methodology for low noise

Kim, K. Y.; Lee, Duck-Joo, KSME, pp.0 - 0, 2005-03

6
Experimental set-up to parallel blade vortex interaction with trailing edge flap at low speed

Baik, K. H.; Lee, Duck-Joo, Americal helicopter society, pp.155 - 161, 2005-11

7
Study on screech tone noise using CAA

Lee, C; Lee, Duck-Joo, ICVFM 2005, ICVFM, 2005-11

8
Computational Aeroacoustics (CAA) : Fundamental and its applications

Lee, Duck-Joo; lee, In Cheol; Kim, Jae Wook; Kim, Young Nam, 6th KSME-JSME TFEC, 2005-03

9
Numerical Investigation of Parallel Blade Vortex Interaction with Split Tip Vortices

Cao, Chi-Hoon; Hwang, Changjeon; Lee, Duck-Joo, 3rd International Conference on Vortex Flows and Vortex Models (ICVFM2005), ICVFM, 2005-11-21

10
Validation of free-vortex embedded CAA method for airfoil vortex interaction

Wie, S.Y.; Cho, C. H.; Lee, Duck-Joo, Americal helicopter society, pp.397 - 403, Acoustical Society of Korea, 2005-11

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