시설
분사기 수류시험 설비
High Mach, High enthalpy, High Reynolds shock tunnel
Driver Tube : Length 3000mm / Dia. 100mm / Maximum Pressure 300bar
Driven Tube : Length 8200mm / Dia. 100mm
Nozzle : Mach ~6.8 / Throat Dia. 32mm / Exit Dia. 340mm / Length 1400mm
Test Section : Length 2400mm / Dia. 1000mm / Pressure 20Pa
Schlieren visualization & BOS measurement
Prediction of flow parameters using PINN-BOS
Planar Laser Scattering (PLS) / Rayleigh Scattering (RS)
Shock interaction / Boundary layer transition
담당자 : 김ㅇㅇ
설비위치 : 몇동 몇호
![569249c97258c800c08e12523efe1b2f](https://fre.snu.ac.kr/wp-content/uploads/sites/9/2023/12/569249c97258c800c08e12523efe1b2f.jpg)
![cc62b0f704bdcd9fca04d8a52b64fe84](https://fre.snu.ac.kr/wp-content/uploads/sites/9/2023/12/cc62b0f704bdcd9fca04d8a52b64fe84.jpg)
단일 분사기 상압 연소시험 설비
High Mach, High enthalpy, High Reynolds shock tunnel
Driver Tube : Length 3000mm / Dia. 100mm / Maximum Pressure 300bar
Driven Tube : Length 8200mm / Dia. 100mm
Nozzle : Mach ~6.8 / Throat Dia. 32mm / Exit Dia. 340mm / Length 1400mm
Test Section : Length 2400mm / Dia. 1000mm / Pressure 20Pa
Schlieren visualization & BOS measurement
Prediction of flow parameters using PINN-BOS
Planar Laser Scattering (PLS) / Rayleigh Scattering (RS)
Shock interaction / Boundary layer transition
담당자 : 김ㅇㅇ
설비위치 : 몇동 몇호
![449484847e1c7b67e43356cedca7a324](https://fre.snu.ac.kr/wp-content/uploads/sites/9/2023/12/449484847e1c7b67e43356cedca7a324.jpg)
![6e49056782e29bb9e457bbc0c9fb91dc](https://fre.snu.ac.kr/wp-content/uploads/sites/9/2023/12/6e49056782e29bb9e457bbc0c9fb91dc.jpg)