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신상준 Shin, Sang Joon

  • - 1985~1989 서울대학교 항공우주공학 학사
  • - 1989~1991 서울대학교 항공우주공학 석사
  • - 1991~1996 국방과학연구소 헬기체계실 연구원
  • - 1996~1999 미국 MIT 항공우주공학 석사
  • - 1999~2001 미국 MIT 항공우주공학 박사
  • - 2001~2003 미국 미시간대학교 항공우주공학과 Post Doctor
Research Interests

In this laboratory, coupled analysis between structural and fluid dynamics is mainly conducted to analyze the aeroelastic characteristics of various vehicles, including turbomachinery. Regarding rotorcraft, CSD/CFD coupled analysis and multidisciplinary design optimization of the active rotor blade such as active trailing edge flaps are being studied. Regarding the fixed-wing aircraft, aeroelastic analysis for the mid/high-altitude unmanned vehicles is being studied. Recently, analysis and experiment for high speed vehicle and its launcher, space launch vehicle, insect-inspired flapping wing micro air vehicle are being conducted. Also, CFD/CSD coupled analysis for turbine blade, EDucation-research Integration through Simulation On the Net(EDISON), rotor blade design and analysis for a delivery drone are being conducted.