Experimental Investigation on Phase Separation of Sprays in Trans- and Super-critical Conditions (dtec.bw Project MaST)
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Summary
Experimental investigation focused on the phase separation of sprays under transcritical and supercritical conditions.
Highly accomplished aerospace engineer with extensive experience in space propulsion, combustion, and fluid dynamics, leveraging deep expertise in experimental and numerical research to advance cutting-edge technologies. Proven leader in academic instruction and international scientific collaboration, with a strong record of impactful publications and patents. Committed to driving innovation and fostering knowledge exchange within the aerospace and mechanical engineering fields.
Space Propulsion, Aerospace Engines, Injectors and Sprays, Combustion, Fluid Dynamics, Thermodynamics, Space Mobility, Advanced Mobility.
Lecturer
München, Bavaria, Germany
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Summary
Delivering advanced academic instruction in space propulsion, shaping the next generation of aerospace engineers.
Highlights
Delivering comprehensive lectures and practical sessions on Space Propulsion (Raumfahrtantriebe) to advanced engineering students, fostering expertise in cutting-edge aerospace technologies.
Research Associate
München, Bavaria, Germany
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Summary
Leading experimental investigations into phase separation of sprays under extreme conditions for the dtec.bw Project (MaST).
Highlights
Led experimental investigations into phase separation of sprays under transcritical and supercritical conditions for the dtec.bw Project (MaST), advancing fundamental understanding of propulsion fluid dynamics.
Designed and constructed a high-pressure and high-temperature testbench, enabling novel experimental setups for extreme condition research.
Implemented advanced optical and laser diagnostics for precise analysis of spray characteristics and combustion phenomena.
Performed rigorous data reduction and conducted comprehensive qualitative and quantitative analyses to derive actionable insights from experimental results, contributing to multiple publications.
Post-Doctoral Researcher
Lampoldshausen, Baden-Württemberg, Germany
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Summary
Executed experimental and numerical research on combustion instability and data analysis for rocket combustors.
Highlights
Conducted experimental and numerical research on injector-driven combustion instability in BKD research rocket combustors, identifying critical parameters for stable operation.
Analyzed extensive data on low-frequency combustion instability from the LUMEN Methane rocket combustor, contributing to design improvements for enhanced reliability and performance.
Collaborated with international teams on propulsion system optimization, contributing to advancements in space propulsion technology.
Post-Doctoral Researcher
Goyang, Gyeonggi-do, Korea (Republic of)
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Summary
Contributed to five research projects focused on aerospace propulsion systems, including rocket and gas-turbine engines.
Highlights
Actively participated in 5 distinct research projects focusing on advanced aerospace propulsion systems, including rocket and gas-turbine engines, contributing to project milestones and deliverables.
Conducted experiments and data collection for propulsion system performance analysis, supporting ongoing research initiatives.
Prepared technical reports and presentations summarizing research findings, facilitating knowledge dissemination within the research group.
Lecturer
Goyang, Gyeonggi-do, Korea (Republic of)
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Summary
Provided specialized instruction in combustion engineering to aerospace students.
Highlights
Delivered specialized lectures on Combustion principles to aerospace engineering students, enhancing their foundational knowledge in propulsion systems.
Guided students through complex theoretical concepts and practical applications of combustion, preparing them for advanced studies and industry roles.
Organizer
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Summary
Organizing initiatives for the Advanced Mobility Expert Network, fostering collaboration of academia and industry.
Highlights
Organizes key initiatives and events for AMExNet, promoting knowledge exchange and networking among mobility experts.
Session Chair
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Summary
Chairing sessions in Mechanical and Aerospace Technology at a prominent international conference.
Highlights
Chairs sessions in Mechanical and Aerospace Technology at the Europe-Korea Conference on Science and Technology, facilitating expert discussions and presentations among international researchers.
Member
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Summary
Advising on aerospace systems, engineering, and technology for K-TAG.
Highlights
Provides expert advisory services on Aerospace Systems, Engineering, and Technology as a member of the Korea Technology Advisory Group (K-TAG) by KIAT, influencing national technology roadmaps.
General Affairs Director
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Summary
Managing general affairs for the European Korean Association of Mechatronics and Aerospace.
Highlights
Oversees general affairs for EKAMA, facilitating operational efficiency and member engagement across European and Korean scientific communities.
Leader of Mechanical Engineering Group
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Summary
Leading the Mechanical Engineering Group and organizing events for 220 members.
Highlights
Leads the Mechanical Engineering Group for VeKNI e.V., organizing workshops and seminars for 220 members to foster professional development and networking.
Member of Supporters
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Summary
Contributing to the dissemination of EU aerospace research and policy trends.
Highlights
Publishes EU trend reports on research and policies in the aerospace field, informing strategic discussions and fostering international collaboration.
Local Committee Member
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Summary
Served as a Local Committee Member for the EKC 2023, supporting an event that attracted approximately 800 participants.
Highlights
Contributed as a Local Committee Member for the Europe-Korea Conference on Science and Technology 2023 (EKC 2023), successfully supporting an event that attracted approximately 800 participants.
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Habilitation
Thermodynamics
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Ph.D.
Aerospace and Mechanical Engineering
Courses
Dissertation: Correlations between Spray and Combustion Characteristics of a Movable Pintle Injector for Liquid Rocket Engines
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M.E.
Aerospace and Mechanical Engineering
Courses
Thesis: Optimal Design Methods for Regenerative-cooled Combustor and Fuel-rich Gas-generator of Liquid Rocket Engine
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B.E.
Aerospace and Mechanical Engineering
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Summary
Experimental investigation focused on the phase separation of sprays under transcritical and supercritical conditions.
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Summary
Post-doctoral research at DLR investigating combustion instabilities in liquid propellant rocket engines induced by fluid-mechanical driving sources in the primary injector.
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Summary
Contribution to the Aerospace Parts and Technology Development Program for a 25kN aero gas turbine combustor.
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Research under the Space Core Technology Development Program on using fluidic baffles to suppress transverse disturbance propagation in liquid rocket combustors.
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Basic Science Research Program focused on the phase change and jet breakup characteristics of heterogeneous hydrocarbon mixtures in supercritical environments.
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Summary
Research at the Advanced Space Propulsion Research Center on the spray and combustion characteristics of pintle injectors for variable thrust rockets.
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Summary
Research under the Space Core Technology Development Program on the combustion of gas-liquid propellants in supercritical conditions.
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Experimental research focusing on the internal flow dynamics of solid rocket motors.
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Summary
Experimental study on pulse detonation engines as part of the NRF(Korea)-RFBR(Russia) Joint Research Program, focusing on fundamentals of modern thrust generators.
Published by
12th European Combustion Meeting
Summary
Presented methods for deconvoluting infrared spray images using optical depth from shadowgraphy.
Published by
Thermodynamik-Kolloquium 2024
Summary
Presented microscopic observations of fuel droplet phase changes in extreme high-pressure and high-temperature environments.
Published by
31. Fachtagung "Experimentelle Strömungsmechanik"
Summary
Discussed macroscopic fuel spray characteristics under sub/transcritical injection conditions.
Published by
Europe-Korea Conference on Science and Technology 2024
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Discussed the environmental impact of rocket launches in the context of the new space era.
Published by
Europe-Korea Conference on Science and Technology 2024
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Presented dynamic spectral analysis techniques for transcritical sprays.
Published by
The Combustion Institute's 40th International Symposium
Summary
Presented findings on near-critical phase changes of cyclopentane droplets in a supercritical nitrogen environment.
Published by
21st International Symposium on Application of Laser and Imaging Techniques to Fluid Mechanics
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Discussed integrated optical diagnostics for characterizing transcritical phase transitions in cyclopentane sprays.
Published by
31. Deutscher Flammentag für nachhaltige Verbrennung
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Compared various imaging methods for analyzing transcritical sprays.
Published by
ILASS Europe 2023, 32nd Conference on Liquid Atomization & Spray Systems
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Presented experimental and numerical investigations of cyclopentane sprays in a transcritical environment.
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ILASS Europe 2023, 32nd Conference on Liquid Atomization & Spray Systems
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Demonstrated the application of machine learning approaches to model the temporal evolution of fuel sprays.
Published by
Europe-Korea Conference on Science and Technology 2023
Summary
Discussed phase change characteristics of cyclopentane droplets at near-critical conditions.
Published by
11th European Combustion Meeting (ECM 2023)
Summary
Presented optical characterization methods for sub- and transcritical fuel sprays using various imaging techniques.
Published by
Physics of Fluids
Summary
Conducted experimental and modeling analysis of transient cyclopentane spray characteristics using machine learning.
Published by
Thermodynamik-Kolloquium 2022
Summary
Detailed investigations of sub- and transcritical fuel spray processes using advanced measurement techniques.
Published by
Europe-Korea Conference on Science and Technology 2022
Summary
Applied spectral analysis to multi-dimensional periodic data for understanding rocket combustion instability.
Published by
Europe-Korea Conference on Science and Technology 2022
Summary
Presented optical diagnostics techniques for fuel sprays in high-pressure and high-temperature chambers.
Published by
19th International Symposium on Flow Visualization (ISFV-19)
Summary
Presented visualizations of cavitation and periodical flow fluctuations originating from a rocket injector orifice.
Published by
Symposium on Thermoacoustics in Combustion: Industry meets Academia (SoTiC 2020)
Summary
Conducted an experimental study on intra-injector flow fluctuations induced by a LOX injector orifice driving combustion instability.
Published by
AIAA Propulsion and Energy 2021 Forum
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Performed a numerical study on acoustic resonance in a LOX injector post induced by orifice flow.
Published by
ODAS(ONERA-DLR Aerospace Symposium)-MOTAR(Measurement and Optical Techniques for Aerospace Research) 2021
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Presented velocimetry measurements of a LOX jet in a high-pressure combustion field using high-speed flame images.
Published by
1st Aerospace Europe Conference (AEC2020)
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Characterized acoustically coupled flow field dynamics using high-speed imaging in high-pressure rocket thrust chambers.
Published by
1st Aerospace Europe Conference (AEC2020)
Summary
Analyzed combustion stability characteristics of sub-scale LOX/LNG rocket thrust chambers.
Published by
38th International Symposium on Combustion 2020
Summary
Detailed the measurement of velocity fields in shear-coaxial, cryogenic flames within high-pressure rocket thrust chambers.
Published by
11th International Symposium on Special Topics in Chemical Propulsion & Energetic Materials 2018
Summary
Presented on the flame structure of gaseous methane/oxygen in a pintle injector.
Published by
Third IAA Symposium of Space Flight Safety 2016
Summary
Conducted a numerical study on the combustion characteristics of fuel-centered pintle injectors for methane rocket engines.
Published by
8th Asian Joint Conference on Propulsion and Power 2016
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Investigated GCH4-air flame characteristics of a pintle injector designed for liquid rocket engines under atmospheric conditions.
Published by
54th AIAA Aerospace Sciences Meeting 2016
Summary
Presented a design procedure for movable pintle injectors for liquid rocket engines.
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12th International Symposium on Experimental and Computational Aerothermodynamics of Internal Flows 2015
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Presented verification of spray simulation for pintle injectors in liquid rocket engines.
Published by
8th Asian-Pacific Conference on Aerospace Technology and Science 2015
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Analyzed cone angle characteristics of pintle injector sprays under atmospheric conditions.
Published by
3rd International Conference on Materials and Reliability 2015
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Conducted a reliability study on the spray performances of pintle injectors for liquid rocket engines using sensitivity analysis.
Published by
66th International Astronautical Congress 2015
Summary
Developed a movable sleeve injector with a fixed pintle for throttleable rocket combustors.
Published by
13th International Conference on Liquid Atomization and Spray Systems 2015
Summary
Investigated the effects of pintle-tip angles on spray characteristics of movable pintle injectors.
Published by
Space Propulsion 2014
Summary
Analyzed flow disturbance characteristics on a fin-slot shaped grain simulator of a solid rocket motor with a submerged nozzle.
Published by
26th European Conference on Liquid Atomization and Spray Systems 2014
Summary
Investigated liquid jet breakup and mixing characteristics from a pintle injector.
Published by
8th China-Japan-Korea Joint Symposium on Optimization of Structural and Mechanical Systems 2014
Summary
Optimized the design of a methane-fuel rocket combustor using a genetic algorithm.
Published by
5th Asian Joint Workshop on Thermophysics and Fluid Science 2014
Summary
Studied liquid sheet breakup caused by gas jet injection from a pintle injector.
Published by
21st International Symposium on Air Breathing Engines Conference 2013
Summary
Investigated the detonation characteristics of acetylene-oxygen with additional liquid fuel.
Published by
24th International Colloquium on the Dynamics of Explosions and Reactive Systems 2013
Summary
Conducted a fundamental study on detonation wave characteristics of acetylene-oxygen mixtures for pulse detonation engines.
Published by
Asian Joint Conference on Propulsion and Power 2012
Summary
Developed design methods for kerosene fuel-rich gas-generators and preburners.
Published by
2nd International Conference on Computational Design in Engineering 2012
Summary
Developed a computational design method for the main combustor profile and regenerative cooling channel shape of liquid rocket engines.
Published by
Hong Kong International Conference on Engineering and Applied Science 2012
Summary
Conducted an experimental study on detonation characteristics of acetylene and oxygen mixtures.