Ph.D. Course

  • Name : 김덕민 [Kim Duk Min]
  • E-mail : kdmin93@naver.com
  • Research : Hypersonic/Supersonic Flow Control Exp. & CFD., Aerothermodynamic, Detonation Flow
  • Publication
  1. Kim, D. M., Lee, H. J. (2024). Estimation of flammable region through experimental observation of liquid hydrogen cloud leaked under various atmospheric conditions. International Journal of Hydrogen Energy.
  2. Kim, D. M., Kim, Y., Roh, T. S., & Lee, H. J. (2022). Observation of unsteady motion induced by counterflow jet on blunt body in hypersonic flow. Journal of Visualization, 25(1), 1-14.
  3. Kim, D. M., Nam, J., Lee, H. J., Noh, K. H., Lee, D., & Kang, D. G. (2020). Study of base DRAG prediction with chamber pressure at super-sonic flow. Journal of the Korean Society for Aeronautical & Space Sciences, 48(11), 849-859.
  • Conference
  1. Duk-Min Kim, ,Jinseok Yoo, Hye In Kim, Seungheon Lee, Hyoung Jin Lee. (2023) Preliminary Flight Test Utilizing Small Methane Engine for Reusable Launch Vehicle, 우주발사체기술심포지움.
  2. Duk-Min Kim, Hyoung Jin Lee. (2023). Experimental visualization of boundary layer transition in hypersonic flow, 우주학술대회.
  3. Duk-Min Kim, Yongchan Kim, Tae-Seong Roh, Hyoung Jin Lee, Jaechung Lee, Hwanil Huh. (2021), An observation of unstable flow characteristics induced by counter flow jet on a blunt body in a high-speed flow field, Asian Joint Conference on Propulsion and Power.
  4. Duk-Min Kim, Hyoung-Jin Lee. (2020). Observation of Jetting flow according to various conditions in the Scarfed Nozzle. 항공우주시스템공학회 추계학술대회.
  5. Duk-Min Kim, Hyoung-Jin Lee. (2020). Experimental Study on Base Drag Variation by Power On/Off in Subsonic Wind Tunnel, 항공우주시스템공학회 춘계학술대회.
  6. Duk-Min Kim, Hyoung-Jin Lee. (2019). Drag Reduction Research with Unsteady of Shock Structure by Counter-flowing Jet in Hypersonic Flow, 항공우주시스템공학회 추계학술대회.
  7. Duk-Min Kim, Young-Chan Kim, Hyoung-Jin Lee. (2019). Experimental Investigation on Drag Reduction by Various in Hypersonic Flow Gas Injection. 항공우주시스템공학회 춘계학술대회.
  8. Duk-Min Kim, Young-Chan Kim, Hyoung-Jin Lee. (2018). Experimental Investigation of Drag Reduction by Counter-flow jet in Hypersonic Flow. 항공우주학회 추계학술대회
  • Name : 임건욱[Yim Geon Wook]
  • E-mail : ynte02@naver.com
  • Research : Scramjet combustion / Wind-tunnel operation
  • Publication
  1. Geon Wook Yim, Tae-Seong Roh, Hyoung Jin Lee.(2021).Flow Characteristics in a Supersonic Combustor with a Configuration of a Cavity.Journal of the Korean Society of Propulsion Engineers,25(2),1-11.
  • Conference
  1. Geon-Wook Yim, Tae-Seong Roh, Hyoung Jin Lee.(2019).A Study on the Characteristics of the Vitiated Heater for the Supersonic Combustion Experiment.The Korean Society of Propulsion Engineers,(),33-33.
  2. Geon Wook Yim, Tae-Seong Roh, Hyoung Jin Lee.(2022).Analysis of Flow Characteristics in a Supersonic Combustor with a Configuration of a Cavity and Preliminary Combustion Test.The Korean Society for Aeronautical and Space,(),822-823.
  3. .Geon-Wook Yim, Hyoung Jin Lee.(2022).Hydrogen combustion characteristics in a Supersonic Combustor with a Configuration of a Cavity.The Korean Society of Propulsion Engineers,,(),271-271.
    4.Geon Wook Yim, Hyoung Jin Lee.(2023).Combustion
  4. .Geon Wook Yim, Hyoung Jin Lee.(2023).Combustion Characteristics in a Supersonic Combustor with a Configuration of a Cavity.KOSCO SYMPOSIUM,(),143-144.
  5. Geon Wook Yim, Hyoung Jin Lee.(2023).Behavior of Shock Wave in a Supersonic Combustor with a Configuration of a Cavity.34th ISSW
  6. Geon Wook Yim, Hyoung Jin Lee.(2023).Hydrogen Combustion Characteristics in Cavity-based Supersonic Combustor.29th ICDERS
  • Name : 하동휘[Ha Dong Hwi]
  • E-mail : dkdlwps14@naver.com
  • Research : Hydrogen Rocket Engine / Regenerative Cooling
  • Publication
  1. Ha, D.; Roh, T. S., Yoo, P.H., & Lee, H. J. (2020).  System analysis of expander cycle hydrogen rocket engine. J. Korean Soc. Propuls. Eng. 24(5), 21–33.
  2. Ha, D., Roh, T. S., Huh, H., & Lee, H. J. (2023). Development trend of liquid hydrogen-fueled rocket engines (part 1: performance and operation). International Journal of Aeronautical and Space Sciences, 24(1), 131-145.
  3. Ha, D., Roh, T. S., Huh, H., & Lee, H. J. (2023). Development Trend of Liquid Hydrogen-Fueled Rocket Engines (Part 2: Core Technologies). International Journal of Aeronautical and Space Sciences, 24(1), 146-165.
  • Conference
  1. Ha, D., Roh, T. S., & Lee, H. J. (2019) Mass Estimation of Liquid Rocket with the Propellant and Cycle Type, KSPE Spring Conference
  2. Ha, D., Roh, T. S., & Lee, H. J. (2019) Analysis of Hydrogen-fueled Expander Cycle Engine using Heat transfer analysis, KSPE Fall Conference
  3. Ha, D., Roh, T. S., & Lee, H. J. (2021) Quantifying Gain Analysis Through Optimal Design of SmalI Launch Vehicle with LH2/LOX Expander Cycle Upper Stage Engine, SASE Fall Conference.
  4. Ha, D., Roh, T. S., & Lee, H. J. (2022) A Study on Estimation of Performance Gain for Small Launch Vehicle by Application of Electric Pump Cycle and the Expansion-Deflection(E-D) Nozzle, SASE Fall Conference
  5. Ha, D., Roh, T. S., & Lee, H. J. (2023) Performance Analysis of Small Launch vehicle with Electric Pump Cycle and E-D Nozzle, KSAS Spring Conference
  6. Ha, D., Roh, T. S., & Lee, H. J. (2023) Experimental Study on the Heat Transfer Characteristics of Liquid Hydrogen in Simulation of Regenerative Cooling Channel, SASE Fall Conference
  • Name : 신종민 [Shin Jong Min ]
  • E-mail : gyfhdj2@naver.com
  • Research : Hydrogen Combustion / Low NOx Burner
  • Publication
  1. Jongmin Shin, Tae-Seong Roh, Hyoung Jin Lee. (2022). Comparison of the Semi-empirical Heat Transfer Coefficient for a Liquid Rocket Nozzle with Regenerative Cooling Jacket. Journal of Propulsion and Energy, 3(1), 51-60.
  • Conference
  1. Jongmin Shin, Teawon Noh, Donghwi Ha, Teaseong Roh, Hyoungjin Lee. (2020). Selection and Evaluation of Empirical Heat Transfer Coefficient Equations for Rocket Nozzle Heat Transfer Analysis. KSPE 2020 Fall Conference, (), 346-346.
  2. Jongmin Shin, Minsig Hwang, Teaseong Roh, Hyoungjin Lee.(2021).Design and Test of Hydrogen Thruster with Film Cooling.KSPE 2021 Spring Conference,(),330-330.
  3. Jongmin Shin, Tae-Seong Roh, Hyoung Jin Lee.(2022).Analysis of Propagation Characters and Internal Structure of Statistically Steady Turbulent Premixed Flames.KOSCO Spring SYMPOSIUM,(),211-213.
  4. Jongmin Shin, Taegun Park, Tae-Seong Roh, Hyong Jin Lee.(2023).CH and NOx Tendency Study on H₂-CH₄ Premixed flame by flow speed.KOSCO Spring SYMPOSIUM,(),159-160.
  • Name : 김승민 [Kim Seung Min]
  • E-mail : victorymin7232@gmail.com
  • Research : Gas turbine combustion / Hydrogen burner
  • Publication
  1. Kim, S., Sim, J., Cho, Y., Sung, B. S., & Park, J. (2021). Numerical Study on the Performance and NOx Emission Characteristics of an 800cc MPI Turbocharged SI Engine. Energies, 14(21), 7419.
  • Conference
  1. Seungmin Kim, Woochan Sim, Myunghoon Han, Jungsoo Park.(2021).Numerical study on the Performance and Emission characteristics under 800㏄ MPI Turbo SI engine.한국자동차공학회 춘계학술대회,(),78-79.
  2. Seungmin Kim, Jungsoo Park.(2020).Optimization study on performance for heavy duty CNG engine based on Latin hypercube sampling and numerical method.한국자동차공학회 춘계학술대회,(),83-84.
  • Name : 김혜인[Kim Hye In]
  • E-mail : khi97234@naver.com
  • Research : Liquid Rocket Engine Supply System / Pump Design / M&S
  • Publication
  1. Kim, H.I., Roh, T.-S., Huh, H., Lee, H.J., (2022). Development of Ultra-Low Specific Speed Centrifugal Pumps Design Method for Small Liquid Rocket Engines. Aerospace, 9, 477.
  • Conference
  1. Kim, H.I., Huh, H., Lee, H.J., (2021). Design of a Low Specific Speed Pump for Small Liquid Rocket Engines. KSAS 2021 Spring Conference.
  2. Kim, H.I., Kim, G.Y, Roh, T.-S., Huh, H., Lee, H.J., (2022). Dynamic Modeling and Simulation Validation of a Liquid Rocket Supply System. KSPE 2022 Spring Conference.
  3. Kim, H.I., Roh, T.-S., Lee, H.J., (2022). Composition and Experiment of Propellant Supply System for Model Methane Rocket Engine. KASA 2022 Fall Conference.
  4. Kim, H.I., Seo, J., Ha, D., Roh, T.-S., Huh, H., Lee, H.J., (2022). A Study on the Pump Manufacturing and Dynamic Characteristic of Small Liquid Rocket Engines. KSPE 2023 Fall Conference.
  5. Kim, H.I., Roh, T.-S., Lee, H.J., (2023). Manufacturing on a Small Liquid Rocket Supply System Component using Metal 3D Printing and a Study on System Modeling and Simulation. AJCPP 2023 11th Conference.
  6. Kim, H.I., Kim, G.Y, Roh, T.-S., Huh, H., Lee, H.J., (2023). Propellant Supply System M&S for Thrust Control of Electric-Pump-Fed Cycle Liquid Rocket Engines. . KSAS 2023 Spring Conference.
  • Name : 황민식 [Hwang Min Sig]
  • E-mail : minsique.louis@inha.edu
  • Research : Water Electrolysis Space Propulsion / Catalytic Ignition
  • Publication
  1. Minsig Hwang, Jongmin Shin, Tae-Seong Roh, and Hyoung Jin Lee, (2021). Study on Various Catalytic Conditions for the Ignition of Hydrogen/Oxygen Mixture, J. Korean Soc. Combust., 26(3), 42-50.
  2. Minsig Hwang, Tae-Seong Roh, and Hyoung Jin Lee,(2022). Conceptual Design and Performance Analysis of Water Electrolysis Propulsion System with Catalytic Igniter for CubeSats, Acta Astronautica, 200, 316-328.
  • Conference
  1. Jongmin Shin, Minsig Hwang, Tae-Seong Roh, Hyoung Jin Lee, (2021), Design and Test of Hydrogen Thruster with Film Cooling, 한국추진공학회 춘계학술대회
    – Minsig Hwang, Jongmin Shin, Tae-Seong Roh, Hyoung Jin Lee, (2021), Design of Hydrogen Thruster Applying Catalytic Ignition System, 한국추진공학회 춘계학술대회
  2. Minsig Hwang, Jongmin Shin, Tae-Seong Roh, Hyoung Jin Lee, (2021), Analysis of Hydrogen Catalytic Combustion Characteristics by Catalyst Contitions, 한국연소학회 춘계학술대회
  3. Minsig Hwang, Jongmin Shin, Tae-Seong Roh, Hyoung Jin Lee, (2021), Anaysis of Ignition Characteristics by Oxidation Conditions of Platinum Catalyst, 한국연소학회 추계학술대회
  4. Minsig Hwang, Jongmin Shin, Tae-Seong Roh, Hyoung Jin Lee, (2021), Catalytic Ignition Characteristics for Application of Hydrogen Thruster, APISAT
  5. Minsig Hwang, Tae-Seong Roh, Hyoung Jin Lee, (2022), Conceptual Design of Water ELectrolysis Propulsion System for LEO CubeSats, 항공우주시스템공학회 춘계학술대회
  6. Dong Ho Kim, Minsig Hwang, Hyeun Yoo, KyoungHwan Han, Tae-Seong Roh, Kee Young Choi, Yo Sup Kim, (2022), A Systematic Approach Study on the Contract Based Department (Employment-Guaranteed Type) for Space Security Professionals, 한국군사과학기술학회 종합학술대회
  7. Dong Ho Kim, Minsig Hwang, Hyeun Yoo, KyoungHwan Han, Tae-Seong Roh, Kee Young Choi, Yo Sup Kim, (2022), A Study on the Curriculum of the Contract Based Department (Employment Guaranteed) in a University for Space Security Professionals, 한국항공우주학회 추계학술대회
  8. Minsig Hwang, Tae-Seong Roh, Hyoung Jin Lee, (2022), Conceptual Design of the Water Electrolysis Propulsion with Catalytic Ignition System, APISAT
  9. Minsig Hwang, Tae-Seong Roh, Hyoung Jin Lee, (2023), Study on Hydrogen Catalytic Ignition for Application to Space Propulsion System, AJCPP
  • Name : 유진석 [Yoo Jin Seok ]
  • E-mail : 000@inha.edu
  • Research : Internal / Interior ballistics, Solid rocket motor optimum design
  • Publication
  1. JinSeok Yoo, Dongwon Kang, Tae-Seong Roh, Hyoung Jin Lee.(2022).A Study on the Optimum Design of Finocyl Grain Using Genetic Algorithm.Journal of the Korean Society of Propulsion Engineers,26(3),22-31.
  • Conference
  1. JinSeok Yoo, Tae Seong Roh, Hyoung Jin Lee.(2022).A Study on the Optimum Design of Grain Using Genetic Algorithm.한국추진공학회 학술대회논문집,(),466-466.
  2. JinSeok Yoo, Seok-Hwan Oh, Tae Seong Roh, Hyoung Jin Lee.(2022).A Study on the Optimum Design of Multi Shape Propellants in Interior Ballistics Using Genetic Algorithm.한국추진공학회 학술대회논문집,(),207-207.
  3. Tae Won Noh, JinSeok Yoo, Tae-Sung Roh, Hyoung Jin Lee.(2022).Thermal analysis and verification considering thermal decomposition and ablation of SRM nozzle.한국추진공학회 학술대회논문집,(),163-163.
  • Name : 김영진 [Kim Young Jin ]
  • E-mail : yj1830@naver.com
  • Research : Supersonic & Hypersonic Intake
  • Publication
  1. Kim. Y.J., & Lee, H.J., (2022). Performance Characteristics of Hypersonic External Compression Inlet Using Isentropic Compression Surface. Journal of the Korean Society for Aeronautical and Space Sciences, 50(5), 297-308.
  • Conference
  1. Kim, Y.J., & Lee, H.J., (2021). Study on the Hypersonic Inlet Performance at Off-Design Conditions Through Numerical Simulations. SASE 2021 Fall Conference.
  2. Kim, Y.J., & Lee, H.J., (2021). Study on the Hypersonic Inlet Performance at Off-Design Conditions through Numerical Simulations. 2021 Asia-Pacific International Symposium on Aerospace Technology.
  3. Kim, Y.J., Roh, T.S., & Lee, H.J., (2022). Study on the Hypersonic External Compression Inlet Using Isentropic Compression Surface. KSAS 2022 Spring Conference.
  4. Kim, Y.J., & Lee, H.J., (2022). Conceptual Design of Two-Dimensional Wedge Type Variable Inlet. KSPE 2022 Spring Conference.
  5. Kim, Y.J., & Lee, H.J., (2022). Conceptual Design of Two-Dimensional Variable Inlet. 2022 Asia-Pacific International Symposium on Aerospace Technology.
  6. Kim, Y.J., & Lee, H.J., (2022). Conceptual Design of Wedge Type Variable Inlet. KSPE 2022 Fall Conference.
  7. Kim, Y.J., & Lee, H.J., (2023). A Study on the Conceptual Design of Two-Dimensional Variable Inlet. 2023 Asian Joint Conference on Propulsion and Power.
  8. Kim, Y.J., & Lee, H.J., (2023). Method for Calculating the Required Mass Flow Rate of Combined Propulsion System. KSPE 2023 Spring Conference.
  9. Kim, Y.J., & Lee, H.J., (2023). Analysis of Shock Structure in Supersonic Inlet with Flight Conditions. 2023 International Symposium on Shock Waves.
  • Name : 이승헌 [Lee Seung Heon]
  • E-mail : seungheon9011@gmail.com
  • Research : Gas turbine performance analysis & simulation
  • Publication
  1. Seungheon Lee, Hyoung Jin Lee, Sangjo Kim, Gyujin Na, Jung Hoe Kim, Two Spool Mixed-Flow Turbofan Engine Performance Analysis Modeling, Journal of the Korean Society of Propulsion Engineers,27(1),37-48.
  • Conference
  1. Seungheon Lee, Tae Young Kang, Hyoung Jin Lee, Chang-Kyung Ryoo.(2021), Fault Simulation and Real data Analysis for Fault Diagnosis of Rotor machinery, 한국항공우주학회 추계학술대회, 178-179
  2. Kang Min Yu, Tae Young Kang, Ha Min Jeon, Seoungheon Lee, Chang-Kyung Ryoo, Hyoung Jin Lee.(2021). Fault Detection in Engine Rotor Using Wavelet Transform and K-mean Clustering, 한국항공우주학회 추계학술대회, 580-581
  3. Seungheon Lee, Hyoung Jin Lee, Sangjo Kim, Gyujin Na, Jung Hoe Kim.(2022). Two Spool Mixed-Flow Turbofan Engine Performance Analysis Modeling, 한국추진공학회 추계학술대회, 208-209
  4. Seungheon Lee, Hyoung Jin Lee, Sangjo Kim, Gyujin Na, Jung Hoe Kim.(2023).Simulink Based Two-Spool Mixed-Flow Turbofan Engine Performance Analysis Modeling Validation, The 11th Asian Joint Conference on Propulsion and Power
  5. Seungheon Lee, Hyoung Jin Lee, Sangjo Kim, Gyujin Na, Jung Hoe Kim.(2023). Performance Evaluation of Engine Model according to Performance Map Application Method, 한국군사과학기술학회 종합학술대회,1514-1515
  • Name : 한경환[Han Kyung Hwan]
  • E-mail : hkh1997a@naver.com
  • Research : Liquid Rocket Engine / Film Cooling
  • Publication
  1. Han, K.H., Rho, T.S., Huh, H.I., & Lee, H.J., (2022). Trend Analysis in Upper Stage Engine Development of Space Launch Vehicles. Journal of the Korean Society of Propulsion Engineers, 26(2), 79-95.
  • Conference
  1. Han, K.H., Rho, T.S., Huh, H.I., & Lee, H.J., (2022). Trend in Upper Stage Engine Development of Space Launch Vehicles. SASE 2022 Spring Conference.
  2. Han, K.H., Rho, T.S., & Lee, H.J., (2022). Experimental Study on the Thrust Throttling of Lab-Scale Methane Rocket Engine. KSAS 2022 Fall Conference. 1605-1606.
  3. Han, K.H., Ha, D.H., Rho, T.S., Huh, H.I., & Lee, H.J., (2023). Lab-Scale Expansion-Deflection Nozzle Design for 500N. KSAS 2023 Spring Conference. 317-318.
  4. Han, K.H., Shin, J.M., Lee, S.H. & Lee, H.J., (2023). Thrust Performance Analysis of GCH4-GO2 Lab Scale Rocket Engine with Film Cooling. SASE 2023 Fall Conference.
  5. Han, K.H., Lee, S.H. & Lee, H.J., (2023). Thrust Perdiction of Methane Rocket Engine with Film Cooling. KSPE 2023 Fall Conference.
  • Name : 윤민식[Yun Min Sik]
  • E-mail : rextrx112@naver.com
  • Research :High-Pressure Hydrogen Self-Ignition
  • Publication

 

  • Conference
  1. Yun, M.S., & Lee, H.J., (2022). Effects of Downstream Pressure Conditions on Self-ignition of High Pressurized Hydrogen. KOSCO 2022 Spring Conference.
  2. Yun, M.S., & Lee, H.J., (2022). Effects of Inactive Mixed Gas In Tube on Self-ignition of High Pressurized Hydrogen. KOSCO 2022 Fall Conference.
  3. Yun, M.S., & Lee, H.J., (2023). Effect of Porous Structure at Tube Outlet on Self-ignition of High-Pressure Hydrogen. KOSCO 2023 Spring Conference.
  4. Yun, M.S., & Lee, H.J., (2023). Effects of Porous Structures at Pipe Outlet on Self-ignition of High-Pressure Hydrogen Leakage. Proceedings of the 29th International Colloquium on the Dynamics of Explosions and Reactive Systems, Paper 163, 2023.