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Junsok Yi
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Year
Adjoint-based design optimization of vortex generator in an s-shaped subsonic inlet
JS Yi, C Kim, BJ Lee
AIAA journal 50 (11), 2492-2507, 2012
392012
Two-scale methodology for URANS/large eddy simulation solutions of unsteady turbomachinery flows
L He, J Yi
Journal of Turbomachinery 139 (10), 101012, 2017
192017
Modeling of axial compressor with large tip clearances
S Evans, J Yi, S Nolan, L Joseph, M Ni, S Kulkarni
Journal of Turbomachinery 143 (6), 061007, 2021
152021
Effects of angles of attack and throttling conditions on Supersonic Inlet Buzz
HJ Namkoung, W Hong, JM Kim, JS Yi, C Kim
The Korean Society for Aeronautical & Space Sciences, 2012
92012
e-AIRS: Construction of an aerodynamic integrated research system on the e-science infrastructure
JH Kim, JS Yi, SH Ko, JW Ahn, CA Kim, YH Kim, KW Cho
Journal of the Korean Society for Aeronautical & Space Sciences 36 (5), 428-437, 2008
92008
Adjoint-based sensitivity analysis for unsteady bladerow interaction using space–time gradient method
J Yi, L Capone
Journal of Turbomachinery 139 (11), 111008, 2017
72017
Space–time gradient method for unsteady bladerow interaction—Part II: Further validation, clocking, and multidisturbance effect
L He, J Yi, P Adami, L Capone
Journal of Turbomachinery 137 (12), 121004, 2015
72015
Space–time gradient method for unsteady bladerow interaction—Part I: Basic methodology and verification
J Yi, L He
Journal of Turbomachinery 137 (11), 111008, 2015
72015
Design Optimization of Vortex Generators for a Junction Vortex of Wing-Body Configuration by Discrete Adjoint Approach
JS Yi, C Kim
51st AIAA Aerospace Sciences Meeting including the New Horizons Forum and …, 2013
62013
Efficient Design Optimization of Vortex Generators in Subsonic Offset Inlet by Discrete Adjoint Approach
J Yi, BJ Lee, C Kim
& Proceedings 저널· 프로시딩즈| 기술보고서| 해외연구초록| Reference DB| 공학 …, 2011
52011
Transient time aeroelastic analysis for a supersonic flight vehicle with a ramjet engine
JY Kwak, W Hong, SJ Shin, I Lee, JS Yi, C Kim
42nd AIAA Fluid Dynamics Conference and Exhibit, 3271, 2012
42012
Aerodynamic Shape Optimization Using Discrete Adjoint Formulation based on Overset Mesh System
BJ Lee, JW Yim, JS Yi, C Kim
KSAS International Journal 8 (1), 95-114, 2007
4*2007
CFD Researches on the e-AIRS: Korean e-Science Aerospace Research System
SH Ko, J Kim, JW Ahn, JS Yi, C Kim, Y Kim, KW Cho, DH Choi
2007 International Conference on Convergence Information Technology (ICCIT …, 2007
32007
Large Eddy Simulation of an Open Rotor Fan Blade
S Priebe, T Wood, J Yi, A Mousavi
Turbo Expo: Power for Land, Sea, and Air 86090, V10AT29A009, 2022
2022
Simulation of rotor-stator flow interaction
YI Junsok, L He, P Adami
US Patent 10,496,769, 2019
2019
Space⤓Time Gradient Method for Unsteady Bladerow Interaction⤔ Part II: Further Validation, Clocking, and Multidisturbance Effect
L He, J Yi, P Adami, L Capone
The American Society of Mechanical Engineers (ASME), 2015
2015
IMPROVEMENT OF VORTEX GENERATOR SOURCE MODEL FOR ADJOINT-BASED DESIGN OPTIMIZATION
S Yi, C Kim
한국산업응용수학회 학술대회 논문집, 2012
2012
Aerodynamic Shape Optimization using Discrete Adjoint Approach On Overset Mesh System
BJ Lee, JW Yim, JS Yi, C Kim
한국항공우주학회, 2007
2007
Spiraling grooves as a hub treatment for cantilevered stators in compressors
Numerical Study on Supersonic Inlet Buzz for Various Flight Conditions
HJ Namkoung, W Hong, JM Kim, JS Yi, C Kim
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Articles 1–20