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- W2944847612 abstract "An array of subsonic counter-flow jets is studied as an active thermal protection system (TPS) for wing leading edges of hypersonic vehicles. The performance is numerically estimated in the model case of a circular cylinder on the basis of the 2D compressible Navier-Stokes equations. In contrast to a single subsonic jet, an array of jets is robust against variation of the angle of attack; high cooling effectiveness is confirmed up to 5° variation. The coolant gas (air) discharged from channels embedded in the cylinder covers over a wide range of the front surface of the cylinder. The feasibility of the active TPS is also discussed." @default.
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- W2944847612 date "2019-01-30" @default.
- W2944847612 modified "2023-09-23" @default.
- W2944847612 title "Numerical investigation of an active TPS for a wing leading edge exposed to high temperature air behind a strong bow shock wave" @default.
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- W2944847612 doi "https://doi.org/10.1186/s42774-019-0001-z" @default.
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