This article deals with the research performed in the framework of the inte
rnal ONERA Hyperenthalpic Hypersonic Project. This project involved fifteen
researchers specialised in different domains, which are the following: fun
damental studies on shock/wave and shock/boundary layers interactions; stud
y of the laminar/turbulent transition; real gas effects and associated phys
ical modelling; the development of non-intrusive optical diagnostic methods
usable in cold and hot wind tunnels; dow rebuilding in a hot shot wind tun
nel such as F4; conception, realisation and validation of computational flu
id dynamics (CFD) solvers. (C) 2000 Editions scientifiques et medicales Els
evier SAS.