The interaction between a shock wave (attached to a wedge) and small a
mplitude, three-dimensional disturbances of a uniform, supersonic, fre
estream flow are investigated. The paper extends the two-dimensional s
tudy of Duck et al. [P W. Duck, D. G. Lasseigne, and M. Y. Hussaini, '
'On the interaction between the shock wave attached to a wedge and fre
estream disturbances,'' Theor. Comput. Fluid Dyn. 7, 119 (1995) (also
ICASE Report No. 93-61)] through the use of vector potentials, which r
ender the problem tractable by the same techniques as in the two-dimen
sional case, in particular by expansion of the solution by means of a
Fourier-Bessel series, in appropriately chosen coordinates. Results ar
e presented for specific classes of freestream disturbances, and the s
tudy shows conclusively that the shock is stable to all classes of dis
turbances (i.e., time periodic perturbations to the shock do not grow
downstream), provided the flow downstream of the shock is supersonic (
loosely corresponding to the weak shock solution). This is shown from
our numerical results and also by asymptotic analysis of the Fourier-B
essel series, valid far downstream of the shock. (C) 1997 American Ins
titute of Physics.