Browse "Dept. of Aerospace Engineering(항공우주공학과)" by Author 618

Showing results 80 to 139 of 240

80
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

81
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

82
Multibody Acoustic Scattering by Using a BEM

Lee, Duck-Joo; Lee, K. D., pp.123 - 129, 1991-05

83
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

84
Noise Prediction of Axial Fan with Rotating Shroud

Kim, Kyu Young; Lee, Duck-Joo, AHS Specialists’ Conference, 2007-10-21

85
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

86
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

87
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

88
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

89
Numerical Investigation of Rotor Wake in Vertical and Forward Flight

Wie, Seong-Yong; Lee, S.; Lee, Duck-Joo, 4th International Conference on vortex flows and models (ICVFM2008, ICVFM, 2008-04-21

90
Numerical investigation of the cover-plates effects on the rectangular open cavity

Heo, Dae Nyoung; Lee, Duck-Joo, 7th AIAA/CEAS Aeroacoustics Conference, 2001-05

91
Numerical investigations of parallel BVI noise with split tip vortices

Cho, C.H.; Lee, Duck-Joo; Hwang, C., AHS Internaitonal 62nd Annual Forum, v.I, pp.13 - 19, American Helicopter Society, 2006-05-09

92
Numerical Prediction of I.C.Engine Intake Noise with a Moving Piston and a Valve

Kim, Y. S.; Lee, Duck-Joo, , 1999-06-01

93
Numerical Prediction of Rotor Tip Vortex Roll-Up in Axial Flight by Using a Time-Marching Tre-Wake Method

Lee, Duck-Joo, International Conference on Vortex Methods, 1999-11-01

94
Numerical Predictions of Acoustic Wave Propagation and Radiation through a Semi-Infinite Tunnel

Lee, Duck-Joo; Hwang, C. J., The 6th Asian Congress of Fluid Mechanics, 1995-05

95
Numerical Simulation of Acoustic Wave Propagation through a Moving Medium at Transonic Speed

Lee, Duck-Joo; Hwang, C. J.; Ko, D. K., The Fifth Asian Congress of Fluid Mechanics, pp.570 - 574, 1992-08

96
Numerical Simulation of Evolutions of a Vortex Ring and Its Interactions with a Rigid Sphere

Lee, Duck-Joo; Ryu, K. W., , 1994-09

97
Numerical Simulation of Scattering Problems by Using a Boundary-Element-Method

Lee, Duck-Joo; Lee, K. D., , 1991-12

98
Numerical Simulation of Sound Generation and Radiation of Intake System by Using Essentially Non-oscillatory Schemes

Lee, Duck-Joo, 5th AIAA/CEAS Aeroacoustics Conference and Exhibit, v.0, no.0, pp.0 - 0, 1999-01

99
Numerical Simulation of Subsonic Inviscid Flow past a Cone Using High-Order Finite Difference Schemes

Kim, J. W.; Lee, Duck-Joo; Morris, P. J., Korea-Japan Joint Symposium: JSASS 16th International Sessions, 2002-10

100
Numerical Simulation of Supersonic Screech Tone Noise using Highorder, High-resolution Optimized Compact Scheme

Lee, In Cheol; Lee, Duck-Joo, Parallel CFD 2006, Parallel CFD 2006, 2006

101
Numerical Simulations of High Speed Train Impulsive Noise Using an Unsteady Deforming Mesh Algorithm

Hwang, C. J.; Lee, Duck-Joo, 16th AIAA Aeroacoustics Conference, pp.65 - 74, AIAA, 1995-06

102
Numerical Simulations of Two-Dimensional Vortex-Body Interaction Using a Vortex Method

Lee, Duck-Joo; Park, J. H., The 3rd JSME-KSME Fluids Engineering Conference, 1994-07

103
Numerical Study of Sound Generation Due to a Spinning Vortex Pair

Lee, Duck-Joo; Koo, S. O., 15th Aeroacoustics Conference, 1993-10

104
Numerical Study of Vortex-Wedge Interaction

Lee, Duck-Joo; Kim, Y. N.; Park, J. H., AIAA 13th Aeroacoustics Conference, AIAA, 1990-10

105
Numerical study on mode transition of open cavity with lids

Heo, D. N.; Kim, J. W.; Lee, Duck-Joo, ASK/KSNVE, 2003-08

106
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

107
Numerical Study on the Radiation of Intake Noise from Internal Combustion by using Essentially Non-Oscillatory Schemes

Kim, Y. S.; Lee, Duck-Joo, International Congress on Sound and Vibration , 1997

108
Numerical Study on Unsteady Transonic Flow Field due to External Excitations

Lee, Duck-Joo; Hwang, C. J., pp.122 - 177, 1991-05

109
Numerical visualization of generation and radiation of intake noise from internal combustion engine by using essentially nonoscillatory schemes

Lee, Duck-Joo; Kim, Y. S.; Chae, K. S., Internoise 98, 1998

110
On the generations of whistle noise from an airfoil and a simplified side mirror

Lee, Y.W.; Cho, C.H.; Lee, Duck-Joo; Lee, I.C., 15th AIAA/CEAS Aeroacoustics Conference (30th AIAA Aeroacoustics Conference), v.5, pp.3387 - 3402, American Institute of Aeronautics and Astronautics, 2009-05-11

111
Optimized Compact Finite Difference Scheme

Lee, Duck-Joo; Kim, J. W., First Asian Computational Fluid Dynamics Conference, 1995-01-01

112
Optimized Compact Finite Difference Schemes for Maximum Resolution Characteristics

김재욱; 이덕주, 94 추계 한국 한국항공우주학회 학술대회, pp.197 - 202, 한국항공우주학회, 1994

113
Optimized Compact Finite Difference Schemes for Solving Wave Equations

Kim, J. W.; Lee, Duck-Joo, 16th AIAA Aeroacoustic Conference, AIAA, 1996-06

114
Optimized High-Order Compact Schemes for Linear and Nonlinear Wave Generation and Propagation

Kim, J. W.; Lee, Duck-Joo, pp.905 - 912, 1996-07

115
Parameter Study of Low Noise CROR System

Yi, Seulgi; Kwon, Hyung Il; Choi, Seongim; Park, Min Jun; Lee, Duck Joo, AIAA Aviation 2016, AIAA, 2016-06-15

116
Prediction of Fuselage Surface Pressure in Rotor-Fuselage Interactions Using an Integral Formulation of Poisson Equation

Jang, Ji Sung; Park, Se Hwan; Lee, Duck-Joo, The 2nd Asian/Australian Rotorcraft Forum and The 4th International Basic Research Conference on Rotorcraft Technology, pp.64 - 72, ARF International Executive Committee, 2013-09-10

117
Prediction of Helicopter Noise and Loading

Lee, Duck-Joo; Jung, C. M., KSASS, pp.221 - 226, 1991-10-01

118
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

119
Prediction of Wake Structure and Induced Velocity of a Helicopter Rotor in Descent Flights using a Vortex Particle Method

Lee, Duck-Joo; Park, SH, ICVFM Nagoya 2014, ICVFM, 2014-11-18

120
Prediction of Wind Turbine Broadband Noise Using Time Marching Freewake Method and Semi-empirical Equation

Lee, Yongwoo; Jang, Ji Sung; Lee, Duck-Joo; Yang, Seung-Un, 1st Asian/Australian rotorcraft forum and Exhibition, ARF2012 Executive Committee, 2012-02-14

121
Predictions of Air Loadings and Wake Structures of Rotating Blades in Vertical Flights by Using Time-Marching Free-Wake Method Strongly Coupled with Nonlinear Rotor Dymanics

Na, Seon UK; Chung, Ki Hoon; Lee, Duck-Joo, Heli Japan 98, pp.333 - 342, 1998

122
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

123
Predictions of Helicopter Wake Geometry and Air Loadings by Using a Time Marching Free Wake Method

Lee, Duck-Joo; Na, S. U., 1st Russia Helicopter Society, pp.69 - 85, 1994-09

124
Predictions of Unsteady-Loading Noise for Slowly Descent Flights with a Time-Marching Free-Wake and Articulated Rotor

Na, S. W.; Chung, K. H.; Chung, C. M.; Lee, Duck-Joo, AHS International Technical Specialist Meeting , 1997

125
Separation on the Flat Plate due to an External Airfoil

Lee, Duck-Joo; Park, J. H., KSASS-Spring, pp.109 - 116, 1990-05

126
Simulations of BVI noise generation using Computational Aeroacoustics

Cho, C.H.; Lee, Duck-Joo; Yu, Y.H., Internoise 2006, pp.0 - 0, Inter-Noise, 2006-12

127
Sound Generation and Radiation from Rotor Tip-Vortex Pairing Phenomenon

Chung, Ki-Hoon; Ryu, Ki-Wahn; Lee, Duck-Joo, 57th AHS Annual From, 2001-05

128
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

129
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

130
Study on blast noise in supersonic flow

Lee, Duck-Joo; Lee, I. C.; Ko, S. H.; Woo, S. D.; Kang, K. J.; Kim, I. W., International Institute of noise control enginering, pp.0 - 0, Inter-Noise, 2005-08

131
Study on Geometric Characteristics and Grid Generation for 3-D Acoustics and Flow Calculation by Using F.D.M.

Hwang, C. J.; Ku, S. O.; Duck Joo Lee, KSASS-Spring, pp.143 - 152, 1990-05

132
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

133
Study on noise characteristics of open cavity with cross-correlation analysis

Heo, D. N.; Kim, J. W.; Lee, Duck-Joo, The Fifth JSME-KSME Fluids Engineering Conference, pp.18 - 20, 2002-10-01

134
Surface Pressure Fluctuations due to Impinging Vortical Flows upon an Airfoil

Lee, Duck-Joo, 1st National Fluid Dynamics Congress, pp.303 - 310, 1988-07

135
Third Order Uniformly Non-Oscillatory Schemes with Modified ACM Technique for Linear Wave and Euler Equcation

Lee, Duck-Joo, AIAA, 1996

136
Third Order UNO Schemes with an ACM for Linear Waves and Euler Equations

Ko, D. K.; Lee, Duck-Joo, The 5th International Symposium on Computational Fluid Dynamics, 1993-09

137
Time Spectral Method 와 Sliding Mesh를 이용한 블레이드 주위의 유동해석

Yi, Seulgi; Lee, Duck Joo; Choi, Seong Im; Im, Dong Kyun, 한국항공우주학회 춘계학술대회, 한국항공우주학회, 2016-04-22

138
Time-domain simulation of nonlinear acoustic propagation in a lined duct

Cho, C.H.; Lee, Duck-Joo; Breard, C.; Premo, J.; Lan, J.H., 14th AIAA/CEAS Aeroacoustics Conference (29th AIAA Aeroacoustics Conference), American Institute of Aeronautics and Astronautics, 2008-05-05

139
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

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