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- W2913502848 abstract "Experimentally simulating the infrared signature of an aircraft with subscale models can significantly reduce the difficulties and costs. The governing equations of fluid flow, heat transfer, and radiation transfer were rendered in only length dimensionless form so that the relationship between infrared signature and scale factor was revealed. Based on the relationship, a method using subscale models to simulate the infrared signature of aircraft was studied. The infrared integrated radiation intensities of four geometrically similar turbofan engine exhaust systems were calculated to validate the simulation measurement method. The results indicate that the parameters of flow field such as velocity, pressure, temperature and mass fraction, as well as the temperatures of walls, are equivalent in the same dimensionless locations in case that the boundary conditions of the geometrically similar models are the same. The relationship between integrated radiation intensity and scale factor is not constant and varies with the aircraft structure and boundary conditions." @default.
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- W2913502848 date "2019-01-01" @default.
- W2913502848 modified "2023-09-28" @default.
- W2913502848 title "A Simulation Method of Aircraft Infrared Signature Measurement with Subscale Models" @default.
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- W2913502848 doi "https://doi.org/10.1016/j.procs.2019.01.177" @default.
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