Showing results 28 to 87 of 240
CAA Application for the Feedback Mechanism in Cavity and Jet Lee, Duck-Joo; Heo, Dae Nyoung; Lee, In Cheol; Kim, Jae Wook, Acoustical society of Japan, pp.1307 - 1310, Acoustical Society of Japan, 2004 |
CAA(Computational Aeroacoustics) : Fundamental and its applications Lee, Duck-Joo; Lee, I. C.; Cho, C. H., Korean-American Scientists and Engineers Association, 2005-08 |
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 |
CFD Simulation and Experimetal Study of Ducted Fan UAV in Hover and Forward Flight Jang, Ji-Sung; Lee, Duck-Joo; Wie, Seong-Yong, 1st Asian/Australian rotorcraft forum and Exhibition, ARF2012 Executive Committee, 2012-02-14 |
CFD-Freewake 연계방법과 중첩격자를 이용한 비정상 로터 해석기법 개발 위성용; 임동균; 권장혁; 이덕주, 2008년 한국항공우주공학회 춘계학술대회, pp.702 - 705, 한국항공우주공학회, 2008-04 |
CFD와 CAA를 연계한 공력소음해석용 기법 개발 허대녕; 이인철; 이덕주; 강국정; 김인우, 2004 한국항공우주학회 추계학술대회, pp.768 - 773, 한국항공우주학회, 2004-11 |
Characterising the aerodynamic and aeroacoustic performance for a small axial-flow fan Cao R.; Lee, Duck-Joo, 2004 ASME Turbo Expo, pp.1699 - 1704, 2004-06-14 |
Characteristic Boundary Conditions and Its Application to Resonance Tube Kwak, S. C.; Rew, H. S.; Lee, Duck-Joo, International Congress on Sonud and Vibration, 1997 |
Characteristic Interface Conditions for Multi-Block High-Order Computation on Singular Structured Grid Kim, J. W.; Lee, Duck-Joo, AIAA/CEAS, 2003-05 |
Characteristics of Acoustic Scattering and Radiation by Arbitrary Two Dimensional Body Shape Lee, Duck-Joo; Lee, K. D., KSASS-Autumn, pp.53 - 60, 1990-10 |
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 |
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 |
Control of Airflow Noise From Diesel Engine Turbocharger Lee, Y.W.; Lee, Duck-Joo; So, Y.; Chung, D., SAE 2011 World Congress and Exhibition, 2011-04-12 |
Correction of Ground Effect for Whirl Tower Test using CFD/Freewake Coupling Method Jang, Ji-Sung; Wie, Seong-Yong; Lee, Duck-Joo; Kwon, Jang-Hyuk; Song, Keun-Woong; Jeong, Ki-Hoon, 1st Asian/Australian rotorcraft forum and Exhibition, ARF2012 Executive Committee, 2012-02-14 |
Cross-correlation 해석을 통한 공동의 소음 특성 연구 허대녕; 김재욱; 이덕주, 대한기계학회 2002년도 학술대회, pp.755 - 758, 대한기계학회, 2002-08-01 |
Development and application of fan noise prediction method to axial and centrifugal fan Lee, Duck-Joo; Jeon, W.H.; Chung, K.H., Proceedings of the 2002 ASME Joint U.S.-European Fluids Engineering Conference, v.257, pp.987 - 992, 2002-07-14 |
Development of a Coupled 2-D Panel/Euler Solver for Numerical Analysis of Transonic Flow Park, Se-Hwan; Lee, Duck-Joo, 1st Asian/Australian rotorcraft forum and Exhibition, ARF2012 Executive Committee, 2012-02-14 |
Development of Adaptive Moving Overset Grid Technique for CAA Lee, Joonseok; Cho, Chi-Hoon; Lee, Duck-Joo, AHS Specialists’ Conference, Korea, 2007, AHS Specialists’ Conference, 2007-10 |
Development of An Efficient Tightly Coupled Euler/Panel Solver for Transonic Flow Analysis Jo, Yeong Min; Park, Se Hwan; Lee, Duck Joo; Choi, Seongim, AIAA Aviation 2016, AIAA, 2016-06-14 |
Development of Fan Performance, Flow and Acoustic Field Analysis Software Lee, Duck-Joo; Jeon, W. H.; Chung, K. H., InterNoise 2000, pp.1521 - 1526, 2000-06-01 |
Direct Simulation of Sound Generation and Radiation from a Singing Wire KIm, J. W.; Lee, Duck-Joo, The 137th Acoustic Society of America, 1999-06 |
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 |
Duct effects on rotor noise in radiation Choi, H.L.; Chung, K.H.; Lee, Duck-Joo, 60th Annual Forum Proceedings - American Helicopter Society, v.2, pp.1968 - 1979, 2004-06-07 |
Effect of Phase Interference on Rotor Thickness Noise Park, S. C.; Lee, Duck-Joo, KSASS-Autumn, pp.195 - 202, 1989-10 |
Effect of Secondary VOrtex on Acoustic Radiation Lee, Duck-Joo; Park, J. H., 93 Inter Noise, 1993-08 |
Effects on Laminar to Turbulent Transition Induced by Highly Accelerated/Decelerated Flow Fields around a Circular Cylinder Seo, Dong-Ho; Lee, Duck-Joo, Asia-Pacific International Symposium on Aerospace Technology 2016, Asia-Pacific International Symposium on Aerospace Technology, 2016-10-26 |
ENO 스킴을 이용한 왕복엔진 흡기계의 소음방사 해석 이덕주, 한국전산유체공학회 1997년도 춘계학술대회, pp.200 - 208, 한국전산유체공학회, 1997 |
Essentially Non-Oscillatory Methods for Shock-Sound Interaction Kim, Y.S.; Lee, Duck-Joo, CAA workshop on Benchmark Problems, 1999-11-01 |
Experimental investigation of noise characteristic of the International Space Station (ISS-RS) Jang, Ji Sung; Lee, Duck-Joo, 60th International Astronautical Congress, 2009, v.1, pp.80 - 85, IAC, 2009-10-12 |
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 |
Experimental Study of a Model Helicopter in Partially Inclined Ground Effect Jang, J.S.; Lee, Duck-Joo, 4th International Conference on vortex flows and models (ICVFM2008), pp.21 - 23, ICVFM, 2008-04 |
Experimental Study of Noise Reduction and Improved Cooling Fan Performance in a PDP TV Kim, K.Y.; Choi, M.G.; Lee, Duck-Joo, Fan-noise 2nd International Symposium, pp.47 - 55, 2003-09 |
Experimental Study of Noise Reduction in a Plasma Display Panel Television Kim, K. Y.; Choi, M. G.; Lee, Duck-Joo, ASK/KSNVE, 2003-08 |
Experimental Study of Ring-wing Type UAV Jang, Ji Sung; Lee, Duck-Joo, 2nd International Forum on Rotorcraft Multidisciplinary Technology, RMT, 2009-10 |
Fan and Rotor Noise Prediction in Frequency Domain Lee, Duck-Joo; Jung, C. M., KSNVE-Spring, pp.111 - 116, 1991-04 |
Fan design methodology for low noise Kim, K. Y.; Lee, Duck-Joo, KSME, pp.0 - 0, 2005-03 |
Flow-tone Generation in an Axisymmetric Whistle Lee, Duck-Joo; Lee, H. K., Inter-Noise Budapest , pp.367 - 370, 1997-08 |
Formulation of Theoretical Relation for Flow Acoustic Feedback inside a Resonator Chindada, Sony; Lee, Duck Joo, 2016년도 춘계학술대회, 한국항공우주학회, 2016-04-22 |
Formulation and Validation of Lighthill-Helmholtz Relation for Scattering Problems in Aeroacoustics Lee, Duck-Joo; Jeon, W. H.; Choi, H. L., 6th AIAA/CEAS Aeroacoustics Conference, 2000-06-01 |
Formulation of Near and Far Acoustic Field from and Incompressible Folw Fluctuation around the Rigid wall 유기완; 이덕주, 수중음향학 학술 발표회, pp.59 - 62, 1996 |
Free vortex embedded 방법을 이용한 Blade Vortex Interaction 해석 위성용; 조치훈; 이덕주, 한국항공우주학회 2005년도 추계학술발표회, pp.1112 - 1115, 한국항공우주학회, 2005-11 |
Generalized Formulation and Application of Characteristic Boundary Conditions Kim, J. W.; Lee, Duck-Joo, 4th AIAA/CEAS Aeroacoustics Conference, Toulouse, 1998 |
High Resolution Free Vortex Blob Method for Highly Distorted Vortex Wake Generated from a Slowly Starting Rotor Blade in Hover Lee, Duck-Joo; Na, S. U., 21th Eropean Rotor Craft Forum, 1995 |
High-Resolution, Nonoscillatory Schemes with Modified ACM Method for Compressible Flow Ko, D. K.; Lee, Duck-Joo, AIAA/CEAS Aeroacoustics Conference, 1996-05 |
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 |
Impulsive Acoustic Wave Generation due to Turbulent Vortex and Lifting Surface Interaction Lee, Duck-Joo, KSASS-Spring, pp.27 - 32, 1988-05 |
Interaction of a Turbulent Vortex with a Lifting Surface Lee, Duck-Joo; Roberts, L., AIAA 23rd Aerospace Science Meeting, AIAA, 1985 |
Interference effect on Rotor Thickness Noise Lee, Duck-Joo; Chung, C. M.; Park, S. C., , 1991-10 |
Investigation of BVI noise generations using Free Wake embedded Computational Aeroacoustics Wie, S.Y.; Chung, K.H.; Lee, Duck-Joo, Heli-Japan, pp.0 - 0, Heli Japan, 2006-11 |
Investigation of Main Rotor-Tail Rotor Interaction in Hover Flight using Vortex Particle Method Park, Se-Hwan; Chu, Yeon Bok; Lee, Duck-Joo, 5th Asian/Australian Rotorcraft Forum, Asian/Australian Rotorcraft Forum, 2016-11-17 |
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 |
Investigation of supersonic jet screech tones using an optimized compact scheme Lee, C.; Lee, Duck-Joo, The 9th Western Pacific Acoustics Conference, WESPAC IX 2006, 2006-06 |
Loss Model과 combined Blade Element 방법을 이용한 팬덕트 테일로터의 성능 해석 및 저소음화 김규영; 이덕주; 정기훈; 강희정, 2004 항공우주학회 추계학술대회, pp.764 - 767, 한국항공우주학회, 2004-11 |
LU-ADI 법을 이용한 3차원 날개 주위의 비점성, 압축성 유동장 해석 황창전; 이덕주; 김명성; 박민우, 92 추계 항공우주학회 학술대회, pp.87 - 90, 한국항공우주학회, 1992-11 |
Multibody Acoustic Scattering by Using a BEM Lee, Duck-Joo; Lee, K. D., pp.123 - 129, 1991-05 |
Noise Generation and Propagation from Subsonic Inviscid Flow past a Cone Kim, J. W.; Lee, Duck-Joo; Morris, P. J., IMA Conference on Computational Aeroacoustics, 2002-04 |
Noise Prediction of Axial Fan with Rotating Shroud Kim, Kyu Young; Lee, Duck-Joo, AHS Specialists’ Conference, 2007-10-21 |
Numerical analysis of a blast wave using CFD-CAA hybrid method Lee, C.; Lee, Duck-Joo, 12th AIAA/CEAS Aeroacoustics Conference, pp.3873 - 3881, American Institute of Aeronautics and Astronautics, 2006-05-08 |
Numerical Computation of Exhaust Noise Through Perforated Diffuser Using Optimized High-Order Compact Schemes Kim, J. W.; Lee, Duck-Joo, International Congress on Sound and Vibration, 1997 |
Numerical investigation about blade vortex interaction using vortex embedded CAA method Wie, S. Y.; Cho, C. H.; Lee, Duck-Joo, The 9th Western Pacific Acoustics Conference, pp.0 - 0, WESPAC IX 2006, 2006-06 |
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