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Sugyeom Kim

Integrated M.S./Ph.D. program

RANS modeling of 3D boundary layers · Synthetic turbulence generation · Radial turbomachinery

B.S. in Mechanical Engineering, Dong-A University, 2025

jjh09jjh@naver.com

PUBLICATIONS

Publications

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2025JOURNAL
Turbomachinery & Aerodynamics

용적형 수소 압축기의 배출 유동에 관한 LBM 기반 유동 및 소음 해석

Doyun An, Junpyo Jin, Sugyeom Kim, Deokjin Jo, 고인재, 이종서, Jin Lee

한국가시화정보학회지 23(1), 37–45

We examine flow and noise in a hydrogen compressor’s valve, jacket, and discharge pipe.

Abstract (original) · EN

To analyze the flow and noise characteristics of a positive displacement hydrogen compressor, a computational fluid dynamics (CFD) simulation based on the Lattice-Boltzmann Method (LBM) was performed. For detailed analysis the discharge flow of the compressor was divided into three regions: the area around the valve, the discharge jacket, and the outlet pipe. Hydrogen passing through the valve formed turbulent jets, which induced high-frequency noise. Inside the discharge jacket, changes in the cross-sectional area caused continuous variations in the average velocity and turbulence characteristics. In the outlet pipe with an elbow, high flow velocity corresponding to the relatively narrow cross-section was observed. Additionally, flow separation occurring on the inner corner of the elbow enhanced turbulence, contributing to the amplification of high-frequency noise. This study provides a physical understanding of the flow and noise issues in positive displacement hydrogen compressors and presents a fundamental analysis to support the design of efficient and low-noise compressors.

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PRESENTATIONS

Presentations & Academic Activities

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2026PRESENTATION
학술대회 초록

국부적인 횡방향 벽면 속도가 존재하는 3차원 난류 경계층 유동에 대한 RANS 모델의 예측 성능 비교 평가

Sugyeom Kim, Jin Lee

제14회 한국유체공학학술대회 (14NCFE) · 2026

Research summary · EN

This study compares k–ω SST, BSL EARSM, and SSG RSM predictions of a three-dimensional turbulent boundary layer subject to localized spanwise wall motion. High-resolution LES provides the reference for assessing shape factor, spanwise wall shear stress, pressure, and turbulent kinetic energy. The comparison examines the accuracy and limitations of the models in transverse-shear flow.

2026PRESENTATION
학술대회 초록

Agentic AI 기반 3D 격자 자동화 및 선택식 댐퍼 오리피스의 유동 특성 매개변수 해석

Excellent Paper AwardKorea Academia-Industrial Cooperation Society, Busan–Ulsan–Gyeongnam Branch ·

Jawoon Hwang, Taeyoung Kim, Seungwoo Son, Sugyeom Kim, Deokjin Jo, Junpyo Jin, Jin Lee

한국산학기술학회 부울경지부 학술대회 · 2026

Research summary · EN

An agentic AI workflow connects geometry modeling, three-dimensional meshing, mesh-quality checks, OpenFOAM setup, solver execution, and postprocessing for selectable damper orifices. Steady laminar simulations vary hole diameter, flow rate, and taper orientation. The abstract reports distinct effects on overall pressure drop and local minimum pressure, motivating their separate assessment in designs intended to suppress cavitation.

2026PRESENTATION
학술대회 초록

NASA CC3 원심압축기의 암모니아 적용에 따른 성능 및 내부 유동 특성 연구

Deokjin Jo, Sugyeom Kim, Seungwoo Son, Taeyoung Kim, Jin Lee

한국산학기술학회 부울경지부 학술대회 · 2026

Research summary · EN

This study evaluates the NASA CC3 centrifugal compressor when ammonia replaces air without a geometry change. Steady compressible RANS simulations in Ansys CFX use the SST k–ω model. Operating conditions are matched using tip Mach number and flow coefficient, with the air performance curve checked against experiments. Pressure ratio, efficiency, work coefficient, shocks, separation, and tip leakage are compared to examine similarity conditions and their limitations.

2026PRESENTATION
학술대회 초록

벤투리관 공동유동에서 공동현상 모형 매개변수 변화에 따른 RANS 예측 민감도 분석

Junpyo Jin, Sugyeom Kim, Jin Lee

한국수소및신에너지학회 추계학술대회 · 2026

Research summary · EN

This study investigates the sensitivity of steady RANS predictions of water–vapor Venturi cavitation to Schnerr–Sauer model parameters. Nuclei number density, nuclei diameter, evaporation coefficient, and condensation coefficient are varied. Cavity length, vapor fraction, pressure drop, and local static pressure are assessed using one-factor sensitivity analysis and Latin hypercube sampling to examine parameter influence, interactions, and assumption-conditioned uncertainty.

2026PRESENTATION
학술대회 초록

액체수소 극저온 밸브 열응력 해석에서 상수 대류열전달계수 가정의 오차 구조

Sugyeom Kim, Deokjin Jo, Junpyo Jin, Jin Lee

한국수소및신에너지학회 추계학술대회 · 2026

Research summary · EN

For a 6-inch liquid-hydrogen globe valve, this study separates errors caused by heat-transfer-coefficient magnitude from errors caused by neglecting its spatial distribution. Three-dimensional RANS and thermal–structural coupling compare local CFD coefficients, an equal-area-average uniform coefficient, and a correlation-based coefficient on the same solid mesh. The reported dominance of coefficient magnitude depends on the thermal-resistance conditions; under external natural convection, external resistance limits both effects.

2026PRESENTATION
학술대회 초록

횡방향 벽면운동으로 유도된 3차원 난류경계층의 RANS 모델링에서 근벽 시간척도 처리의 역할

Sugyeom Kim, Jin Lee

한국전산유체공학회 추계학술대회 · 2026

Research summary · EN

This study examines how near-wall turbulence time-scale treatment affects RANS predictions of a three-dimensional boundary layer induced by localized spanwise wall motion. DNS with digital-filter synthetic inflow provides the reference. OpenFOAM comparisons include standard eddy-viscosity and Reynolds-stress models, ω-based time scales, and mixed ω/ε treatments. Wall-motion increments in mean velocity, Reynolds stresses, and wall shear stress are compared with DNS.

2025PRESENTATION
학술대회 논문·초록

LBM을 이용한 용적형 압축기의 유동 모사

Doyun An, Sugyeom Kim, Deokjin Jo, Junpyo Jin, Jin Lee

Presenter Doyun An

한국가시화정보학회 춘계학술대회 · 2025.04

Research summary · EN

LBM simulations resolve a positive-displacement hydrogen compressor with its cylinder, discharge valves, and outlet passages to examine turbulence and noise.

2024PRESENTATION
학술대회 논문·초록

축류 압축기에서 입구 동압 분포의 영향에 관한 수치적 연구

Sugyeom Kim, Deokjin Jo, Jin Lee

Presenter Sugyeom Kim

대한기계학회 부산지회 추계학술대회 · KSME2024R2073

Research summary · EN

A nonuniform inlet dynamic-pressure profile derived from a boundary layer is applied to NASA Rotor 67, and blade loading and flow behavior are compared with a uniform-inlet case.