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- W4284976281 abstract "The design of the inlet radial distortion generator is the key technology of the compressor component performance test and aerodynamic stability test. This paper designed several radial distortion generators composed of annular metal wires for high-pressure compressor and core engine inlet to simulate the actual total pressure profile of the incoming flow. The design of the radial distortion generator uses the principle of airflow flowing through different metal wires to produce different magnitudes of flow losses to generate the required radial total pressure distribution. Through numerical simulation of wire distortion generations with different diameters, quantities, and arrangements, and iteratively adjusted the generator’s parameters, the total pressure distribution at the target position of the distortion generator finally meets the target design requirements." @default.
- W4284976281 created "2022-07-10" @default.
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- W4284976281 date "2022-07-09" @default.
- W4284976281 modified "2023-10-14" @default.
- W4284976281 title "Design of Aircraft Engine Inlet Radial Distortion Generator" @default.
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- W4284976281 doi "https://doi.org/10.1007/978-981-16-8154-7_14" @default.
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