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- W2330404867 abstract "For the many applications of gas turbine engines installed with APU-style inlets such as unmanned aerial vehicles, auxiliary power units, and helicopters, the inlet swirl distortion created from these complicated inlet systems has become a major performance and operability concern. To improve the design of the APU-style inlet systems, better understanding of the flow field and the mechanism for swirl development is necessary. This paper describes the development of a research facility at Purdue University, in cooperation with Honeywell, that provides relevant flow rates through an APU-style inlet such that detailed measurements can be taken in the flow field. A subcritical air ejector is used to continuously flow the inlet at desired corrected mass flow rates. A PID control method is used to maintain the stable operation of the flow system. The steady performance of this system is quantified, and the method used to improve the operation steadiness is described. The facility provides stable operation of the inlet over a wide range of corrected mass flow rate from 1.0 lbm/s to 5.5 lbm/s, which matches the Reynolds number and Mach number in the real engine operating environments and enables further research in resolving the detailed flow field and understanding of the swirl development inside the APU-style inlet." @default.
- W2330404867 created "2016-06-24" @default.
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- W2330404867 date "2015-06-19" @default.
- W2330404867 modified "2023-09-24" @default.
- W2330404867 title "Development of a Research Facility to Study the Flow Field in an APU-Style Inlet" @default.
- W2330404867 cites W2035807801 @default.
- W2330404867 cites W2006557938 @default.
- W2330404867 doi "https://doi.org/10.2514/6.2015-2860" @default.
- W2330404867 hasPublicationYear "2015" @default.
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