The purpose of this paper is to give the first results of a linear sta
bility analysis which has been applied to the problem of shock oscilla
tions in a transonic diffuser flow. The mean flow is calculated with a
numerical code solving the averaged Navier-Stokes equations, but the
proposed stability approach is limited to the core region where the vi
scous effects can be neglected. In order to validate the present appro
ach, the results are compared with Sajben's experimental results and t
hose numerically obtained by Lieu and Coakley. It is the first time th
at these published results are compared with a simple linear stability
analysis. As demonstrated below, the shock motion spectra have been c
orrectly reproduced and the frequencies of 200 Hz and 300 Hz have been
clearly obtained for the diffuser lengths of l/h = 13 and l/h = 8.6 r
espectively. As far as stability of the mean flow is concerned, the te
mporal amplification rate is always negative, the mean flow is therefo
re linearly stable. Finally, the amplitude and phase of the fluctuatin
g pressure have been compared. The phase for example is in very good a
greement with the experimental results. This can prove that at least i
n some cases, self-sustained shock oscillations can be explained and p
redicted with an inviscid linear stability analysis. (C) Elsevier, Par
is.