이상윤[Lee Sangyoon]

  • Name : 이상윤 [Lee Sangyoon]
  • E-mail : sangyoon.lee@inha.ac.kr
  • Office : 항공 – 405
  • Experience

2025 ~ present           Assistant Professor                 Aerospace Engineering, Inha University

2021 ~ 2025                Senior Researcher                   Korea Aerospace Research Institution

  • 주요 학술 논문
  • 국외 저널
  1. Lee. S., Yun. M.S. & Lee. H.J. (2026). Effect of initial sub-atmospheric extension-tube pressure on ignition and flame development during high-pressure hydrogen release. International Journal of Hydrogen Energy, 280
  2. Jung. H.J., Han. K.H., Lee. S. & Lee. H.J. (2026). Numerical investigation of film cooling hole design effects on the cooling performance of an expansion–deflection nozzle pintle. Aerospace Science and Technology, 176.
  3. Kim. Y.J., Lee. S. & Lee. H.J., (2026). Off-Design Performance of Wavecatcher Intakes  Based on Intake Shapes, AIAA-Journal of Aircraft. 
  4. Kim. J.B, Kim. Y.J., Lee. S. & Lee. H.J. (2025).  Study on the Performance Characteristics of Osculating Cone Waverider According to Shock Wave Angle. International Journal of Aeronautical and Space Sciences, 27, 2586-2605.
  5. Lee, S, Jun, S., Huh, J.S., Park, P. & Lim, B.J. (2024). Inclined installation effect on the offset strip finned heat exchanger designed for a hybrid electric propulsion system in electric vertical take-off and landing. Energies, 17(19), 4960
  6. Lee, S., Roh, T.S. & Lee, H.J. (2023). Influence of jet parameters of fluidic oscillator-type fuel injector on the mixing performance in a supersonic flow field. Aerospace Science and Technology, 134, 108154
  7. Lee, S., Lee, B.J. & Jeung, I.S. (2021). Wavefront distortion due to the shock wave and boundary layer in the supersonic flow over a compression ramp, Aerospace Science and Technology, 110, 106489
  8. Lee, S. & Lee, B.J. (2021). Dynamic and stability of premixed hydrogen-air flames in square micro channels with wall temperature gradients. Proceedings of the Combustion Institute, 38(2), 1933-1943
  9. Han, S., Lee, S. & Lee, B.J. (2020). Numerical analysis of thermochemical nonequilibrium flows in a model scramjet engine. Energies, 13(3), 606
  10. Lee, S., Kim, S.H., Lee, H.J. & Jeung, I.S. (2018). Density acquisition and aero-optics measurement from BOS images for a hot jet, 19(3), 563-574
  11. Development of the arcsecond pico star tracker(APST). Transactions of the Japan Society for Aeronautical and Space Sciences, 60(6), 355-365
  • 국내 학술지
  1. 마이크로 가스터빈 터보제너레이터 기반 하이브리드 전기추진 시스템의 운용 특성 평가 연구, 한국유체기계학회지, 29권, 3호, pp.54-65, 2026
  2. 무인기용 터보제너레이터를 위한 300 N급 마이크로 터보제트 코어 기반 동력터빈 설계, 한국유체기계학회지, 29권, 3호, pp.35-43, 2026
  3. 1,000마력급 터보샤프트엔진 역류형 환형 연소기 성능시험평가 연구. 한국추진공학회지,28권,1호, pp. 46-55, 2024
  4. 스월안정화/코안다 안정화 화염을 적용한 가스터빈 연소기 연소성능 특성에 대한 시험연구, 한국추진공학회지,27권,2호,pp. 10-19, 2023