ILES of an array of three subsonic counter-flow jets issuing from a wing leading edge exposed to hypersonic aerodynamic heating

ILES of an array of three subsonic counter-flow jets issuing from a wing leading edge exposed to hypersonic aerodynamic heating

Abstract The flow of an active thermal protection system exploiting subsonic counter-flow jets for wing leading edges of hypersonic vehicles is numerically studied on the basis of the three dimensional Navier-Stokes equations. The coolant air issuing from around the stagnation point as an array of t...

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Bibliographic Details
Main Authors: Tomonori Shimada, Taku Ohwada
Format: Article
Language:English
Published: SpringerOpen 2020-05-01
Series:Advances in Aerodynamics
Subjects:
Subsonic jet
Counter-flow
Aerodynamic heating
TPS
Rayleigh-Taylor
Kelvin-Helmholtz
Online Access:http://link.springer.com/article/10.1186/s42774-020-00037-8

Internet

http://link.springer.com/article/10.1186/s42774-020-00037-8

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