Data di Pubblicazione:
2009
Abstract:
In the inner part of the dissociated boundary
layer around various bodies in hypersonic flow
regime, a vibrational freezing zone has been
observed. This freezing region takes place even
if , in the outer part of the boundary layer,
translation and vibration temperatures are in
equilibrium and even if the wall may be
considered as catalytic. This phenomenon can
be attributed to the diffusion towards the wall
of vibrationally excited molecules. The
consequence of this behaviour is an increase of
the dissociation rate constants in this region..
The present determination of such rate
constants is carried out for two characteristic
types of boundary layer, behind a reflected
shock wave and close to a stagnation point, by
using various physical models, such as state to
state methods but also global models simpler to
use. All methods can predict the general
features of the freezing phenomenon and
present a qualitative agreement, as far as
similar assumptions are used.
Tipologia CRIS:
04.01 Contributo in Atti di convegno
Elenco autori:
Capitelli, Mario; Armenise, Iole
Link alla scheda completa:
Titolo del libro:
Proceedings of The 6th European Symposium on Aerothermodynamics for Space Vehicles