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- W2013024926 abstract "175.74mm . 터빈 입구에서의 상세 유동이 측정되었다 노즐의 허브면에서 측정한 압력과 노즐의 쉬라우드 면과 터 . 빈 휠 케이싱에서 측정한 압력 분포를 볼 때 터빈 내부에서의 팽창과정이 적절함을 확인할 수 있었다. Abstract: An aerodynamic rig test of a radial turbine for an auxiliary power unit (APU) was performed at a high-temperature turbine test facility at the Korea Aerospace Research Institute. The pressure ratio, Mach number, and flow coefficient in the rig test are the same as those under normal engine operation conditions. The design pressure ratio is 3.096, design test speed is 34909 rpm, and turbine inlet temperature is 160°C. The turbine has airfoil-type nozzles, and the diameter of the turbine wheel is 175.74 mm. The turbine map is experimentally measured, and the detailed flow at the turbine inlet is measured. The pressure distribution in the nozzle at both the hub and the shroud sides and the pressure distribution along the shroud casing of the turbine wheel were measured, and this confirmed that the expansion process in the turbine wheel is acceptable." @default.
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- W2013024926 date "2013-01-01" @default.
- W2013024926 modified "2023-09-27" @default.
- W2013024926 title "Aerodynamic Rig Test of Radial Turbine for APU" @default.
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- W2013024926 doi "https://doi.org/10.3795/ksme-b.2013.37.1.001" @default.
- W2013024926 hasPublicationYear "2013" @default.
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