Numerical investigation of an active TPS for a wing leading edge exposed to high temperature air behind a strong bow shock wave
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 con...
| Main Authors: | , , |
|---|---|
| Format: | Article |
| Language: | English |
| Published: |
SpringerOpen
2019-01-01
|
| Series: | Advances in Aerodynamics |
| Subjects: | |
| Online Access: | http://link.springer.com/article/10.1186/s42774-019-0001-z |