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14744
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2021.02.08
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2023.08.21
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이재인

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이름 : 이재인
E-mail : rokafasnu@snu.ac.kr
연구실번호 : 단재관 326호
연구실 전화번호 : 043-290-5472


경력

▶ 학력
- 2012. 3. ~ 2016. 2. : 공군사관학교 항공우주공학전공 공학사
- 2018. 3. ~ 2020. 2. : 서울대학교 기계항공공학부 우주항공공학전공 공학석사


 
▶ 직위
- 2020. 2. ~ 2021. 2. : 공군사관학교 항공우주공학과 전임강사
- 2021. 2. ~ 2023. 3. : 공군사관학교 항공우주공학과 조교수(일반)
- 2023. 4. ~          : 공군사관학교 항공우주공학과 조교수(전임)
 
▶ 보직
- 2020. 3. ~ 현재 : 공군사관학교 항공우주공학교수
- 2020. 5. ~ 2021. 7 : 공군사관학교 풍동실험실 과제관리 및 실험담당
- 2021. 7. ~ 2022. 6. : 공군사관학교 풍동실험실 과제운영담당

담당과목


압축성 유체역학, 항공역학 및 실험, 항공공학개론, 우주공학개론,
항공우주특성화교육(인공위성운영실습)

연구분야


전산유체역학, 극초음속 공기역학, 스크램제트 복합추진시스템, 풍동실험


학술활동

▶ International Journals

2. Kim, J.S., Kim, K.H. & Lee, J. Improvement of Heat Transfer Model Considering Heat Transfer Deterioration of Supercritical Fluid in Cooling Channel of Scramjet Propulsion System. Int. J. Aeronaut. Space Sci. (2023). 

1. Lee, M., Lee, J., Kim, K. H., & Kim, H. (2021). Efficient Aerodynamic Analysis of Air-Breathing Hypersonic Vehicle using Local Surface Inclination Method based on Unstructured Meshes. International Journal of Aeronautical and Space Sciences, 22(5), 1031-1041. [SCIE]

 

▶ Domestic Journals

4. Lee, J., Cho, D., Lee, Y., Lee, Y., Kim, K, Kim, J. (2023). Multi-DOF Virtual Flight Testing and Free Flight Wind Tunnel Test System Development for Investigation of Aircraft Flight Characteristics. Journal of the Korean Society for Aeronautical & Space Sciences, 51(3), 149-157. [SCOPUS]

3. Lee, S., Shin, J., Lee, J., Kim, J., Kim, S., Kim, S., & Cho, D. (2022). Development of Modeling and Simulation Tool for the Performance Analysis of Pods Mounted on Highly Maneuverable Aircraft. Journal of the Korean Society for Aeronautical & Space Sciences, 50(7), 507-514. [SCOPUS]

2. Lee, J., Shin, J., Cho, D., Jung, H., Choi, T., Lee, J., ... & Kim, S. (2022). Analyses on Aerodynamic and Inertial Loads of an Airborne Pod of High-Performance Fighter Jet. Journal of the Korea Institute of Military Science and Technology, 25(1), 9-22. [KCI]

1. Lee, J., & Kim, K. (2020). Three-dimensional numerical analysis of scramjet cooling channel for one-dimensional model development. Journal of Korean Society of Computational Fluids Engineering, 25(3), 78-86. [KCI]

 

▶ International Conferences

1. Lee, J., Cho, D., Jang, Y. I., & Kim, J. (2022. 6. 27. - 7. 1.). Design of a Multi-DOF Test Platform for the Wind Tunnel based Virtual Flight Testing[Poster presentation]., 9th European Conference for Aeronautics and Space Sciences(EUCASS-3AF), Lille, France

 

▶ Domestic Conferences

6. Jongbum Kim, Jaein Lee, Sanghyun Lee, Donghyun Cho. (2022). Multi-DOF Wind Tunnel Test for Fighter Flight Characteristics Investigation. Korea Institute of Military Science and Technology Conference Proceedings

5. Sanghyun Lee, Jaein Lee, Jongbum Kim, Donghyun Cho, Hyoungseog Chung. (2022). A Study on Improvement of Wind Tunnel Test for Determination of Separated Dynamic Stability Derivatives of Tailless Aircraft. Korea Institute of Military Science and Technology Conference Proceedings

4. Nae- Yeong Noh, Youn- Ha Shin, Dong- Min Lee, Jun- Tae Lee, Jaein Lee. (2021). Mission Profile-based Performance Analysis of Dual-mode Scramjet Variable Inlet. The Korean Society for Aeronautical and Space Sciences Conference Proceedings

3. Jae Seung Kim, Jae In Lee, Kyu Hong Kim. (2020). A Numerical Study and Calibration of One-Dimensional Heat Transfer Model Considering JP-10 Fuel Properties and the Three-Dimensional Effect of Scramjet Cooling Channel. The Korean Society for Aeronautical and Space Sciences Conference Proceedings

2. Jaein Lee, Kyuhong Kim. (2020). Three-Dimensional Numerical Analysis of Scramjet Cooling Channel for One-Dimensional Model Development. The Korean Society for Aeronautical and Space Sciences Conference Proceedings

1. Jaein Lee, Kyu Hong Kim. (2019). Three-Dimensional Numerical Analyses on Heat transfer of hydrocarbon fuel in Scramjet Cooling Channel at Different Channel Aspect Ratio for One-Dimensional Thermal Model. The Korean Society for Propulsion Engineers Conference Proceedings


▶ Technical Reports

7. “Wind Tunnel Test of an Unmanned Aerial Vehicle with Folding Wings” [final], Agency for Defense Development, 2022.8

6. “A Study of the High-Risk Flight and High Angle-of-Attack Test Using KF-X Scaled Model” [interim], Korea Aerospace Industries Co., 2022.05.

5. “Wind Tunnel Test of Propeller Performance of UAV” [final], Agency for Defense Development, 2022.2.

4. “Study on the Aerodynamic Characteristic of UAV by Wind Tunnel Test” [interim], Agency for Defense Development, 2021.9.

3. “A Study of the High-Risk Flight and High Angle-of-Attack Test Using KF-X Scaled Model” [annual], Korea Aerospace Industries Co., 2021.7.

2. “High-Resolution Electro-Optical/Infrared (EO/IR) Payload to be Mounted on a High-Maneuverable Fighter Jet” [final], LIG Nex1 Co., Ltd., 2021.3.

1. “Scramjet Combined Propulsion System” [final], Agency for Defense Development, 2020.12.

 

▶ Projects

7. 스크램제트 추진시스템의 열공력 해석 및 냉각시스템 설계 연구, 국방과학연구소, 2021.7.16.~2024.05.31.

6. 충북 UAM(20%) 풍동실험 연구, 청주대학교, 2022.8.~2022.12.

5. 비행체(UAV) 기본공력 풍동시험, 국방과학연구소, 2022.3.~2022.8.

4. KFX 축소기를 활용한 고받음각/고위험 비행시험연구, 세종대학교(항공우주산업), 2020.10.~2022.12.

3. 비행체(UAV) 기본공력 및 프로펠러 추력측정 풍동시험, 국방과학연구소, 2021.7.~2022.2.

2. 고기동 항공기 탑재 고분해능 영상획득 탑재체 기술연구, LIG넥스원, 2020.4.~2021.5.

1. 스크램제트 추진시스템의 열공력 해석 및 냉각시스템 설계 연구, 국방과학연구소, 2018.12.~2020.1

 

▶ Books

1. 공저, (2020). 우주공학개론(Introduction to Astronautics), 국군인쇄창

 

▶ Memberships & Professional Societies

the Korea Institute of Military Science and Technology (KIMST), 2021~

the Korean Society for Computational Fluids Engineering (KSCFE), 2020~

the Korean Society for Aeronautical and Space Sciences (KSAS), 2020~


▶ Thesis

Master’s Thesis : Three-Dimensional Numerical Analysis on Heat Transfer of Scramjet Cooling Channel at Different Aspect Ratio for One-Dimensional Thermal Model, 2020

직위 또는 학위
조교수
최종학력
서울대학교 기계항공공학부 (공학석사)
전화번호
043-290-5472
연구분야
전산유체역학, 극초음속 공기역학, 스크램제트 복합추진시스템, 풍동실험
연구실
단재관 326호
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