Influence of instability modes on cooling performance in hypersonic boundary layer with slot injection
A combined numerical-experimental investigation is presented with focus on the effects of boundary-layer instabilities and transition on the wall cooling performance in a Mach 5 low-enthalpy flow over a flat plate, with coolant injection achieved through a row of slots. The numerical study has been...
Autors principals: | Cerminara, A, Hermann, T, Ifti, HS, Deiterding, R, Sandham, N, McGilvray, M |
---|---|
Format: | Journal article |
Idioma: | English |
Publicat: |
Elsevier
2020
|
Ítems similars
-
Numerical simulation of transpiration cooling in a laminar hypersonic boundary layer
per: Ifti, HS, et al.
Publicat: (2022) -
Numerical Simulation of Transpiration Cooling in a Laminar Hypersonic Boundary Layer - Dataset
per: Ifti, H S, et al.
Publicat: (2022) -
Quantifying the surface heat transfer on transpiration cooled porous materials in laminar and turbulent hypersonic boundary layers
per: Naved, I, et al.
Publicat: (2022) -
Displacement of hypersonic boundary layer instability and turbulence through transpiration cooling
per: Kerth, P, et al.
Publicat: (2024) -
Laminar transpiration cooling experiments in hypersonic flow
per: Ifti, HS, et al.
Publicat: (2022)