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- W2359085815 abstract "The 3D Reynolds averaged Navier-Stokes equations and model were used to calculate the airflow field around the strut of an aeroengine inlet for the anti -icing. The control equation of subcooling droplet in the air was built and solved by using Eulerian model. The characteristics of droplet impacting on the strut surface were achieved based on some flight conditions, and anti-icing heat load distribution on its surface were also obtained on both complete evaporation and incomplete evaporation. On the basis of the results, the heating configuration and structure of the strut can be designed." @default.
- W2359085815 created "2016-06-24" @default.
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- W2359085815 date "2009-01-01" @default.
- W2359085815 modified "2023-09-22" @default.
- W2359085815 title "Numerical Simulation of Anti-icing Heat Load for Strut of Aeroengine Inlet" @default.
- W2359085815 hasPublicationYear "2009" @default.
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