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Bu-Kyeng Sung
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Design of a Mach 2 shape transition nozzle for lab-scale direct-connect supersonic combustor
BK Sung, JY Choi
Aerospace Science and Technology 117, 106906, 2021
192021
Real-Gas-Flamelet-Model-Based Numerical Simulation and Combustion Instability Analysis of a GH2/LOX Rocket Combustor with Multiple Injectors
WS Hwang, BK Sung, W Han, KY Huh, BJ Lee, HS Han, CH Sohn, ...
Energies 14 (2), 419, 2021
122021
Direct-connect supersonic nozzle design considering the effect of combustion
BK Sung, SM Jeong, JY Choi
Aerospace Science and Technology 133, 108094, 2023
82023
Design of a shape transition nozzle for lab-scale supersonic combustion experimental equipment
BK Sung, WS Hwang, JY Choi
Journal of the Korean Society for Aeronautical & Space Sciences 48 (3), 207-215, 2020
42020
Numerical Simulation of Combustion Instability in a Direct-Connect Supersonic Combustor
SM Jeong, HS Han, BK Sung, ES Lee, JY Choi
AIAA Propulsion and Energy 2021 Forum, 3535, 2021
32021
Numerical Study on the Process of Supersonic Flow Formation in a Direct-Connect Supersonic Combustor
SM Jeong, HS Han, BK Sung, ES Lee, JY Choi
Journal of the Korean Society for Aeronautical & Space Sciences 48 (11), 889-902, 2020
32020
Reactive Flow Dynamics of Low-Frequency Instability in a Scramjet Combustor
SM Jeong, HS Han, BK Sung, W Kim, JY Choi
Aerospace 10 (11), 932, 2023
22023
Investigation of Vitiation Effects in Scramjet Combustor using Hybrid RANS/LES
SM Jeong, J Kim, BK Sung, MS Kim, JY Choi
AIAA SCITECH 2024 Forum, 1418, 2024
2024
Operation Mode Analysis of Dual Combustion Ramjet Engine from 3D Turbulent Combustion Simulation
MS Jo, BK Sung, SM Jeong, JY Choi
AIAA SCITECH 2024 Forum, 1249, 2024
2024
Performance Assessment of Vitiated Air Heater by Numerical Combustion Analysis for Direct-Connect Scramjet Test Facility
BK Sung, SM Jeong, MS Kim, JY Choi
AIAA SCITECH 2024 Forum, 1416, 2024
2024
Reactive Flow Dynamics of Low-Frequency Instability in a Scramjet Combustor. Aerospace 2023, 10, 932
SM Jeong, HS Han, BK Sung, W Kim, JY Choi
2023
Design of Shape Transition Nozzle for Direct-connect Supersonic Combustor
BK Sung, JY Choi
AIAA Propulsion and Energy 2021 Forum, 3539, 2021
2021
Two-phase Flow Study of the RD-0110 Engine Injector with different Recess Lengths
V Natarajan, WS Hwang, BK Sung, JY Choi
AIAA Propulsion and Energy 2021 Forum, 3575, 2021
2021
Direct-Connect 초음속 연소기 내 초음속 유동 형성과정에 대한 수치해석; Direct-Connect 초음속 연소기 내 초음속 유동 형성과정에 대한 수치해석; Numerical Study on the Process of …
SM Jeong, HS Han, BK Sung, ES Lee, JY Choi
Journal of the Korean Society for Aeronautical & Space Sciences 48 (11), 889-902, 2020
2020
소형 초음속 연소시험 장치를 위한 형상 천이 노즐 설계; 소형 초음속 연소시험 장치를 위한 형상 천이 노즐 설계; Design of a Shape Transition Nozzle for Lab-scale Supersonic …
BK Sung, WS Hwang, JY Choi
Journal of the Korean Society for Aeronautical & Space Sciences 48 (3), 207-215, 2020
2020
Numerical Simulation of Film-cooled Vitiated Air Heater for Direct-connect Scramjet Experiment
BK Sung, ES Lee, JH Lee, SM Jeong, JY Choi
3D Numerical Simulation for the Combustion Characteristics Analysis of the Dual Combustion Ramjet Engine
MS Jo, BK Sung, SM Jeong, JY Choi
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