A tutorial summary is given of the theory of aerodynamic sound with sp
ecial reference to the generation of sound by flow interacting with ri
gid and elastic structures. Lighthill's acoustic analogy and the theor
y of vortex sound are discussed. Several applications of the theory ar
e described that exemplify the considerable progress that has been mad
e in the analytical treatment of flow generated sound at low Mach numb
ers, including the use of the compact acoustic Green's function to est
imate fluid-structure interaction noise when one or more pertinent sou
rce dimensions are small compared to the acoustic wavelength. The need
to take proper account of additional sources formed by vortex sheddin
g during an interaction is emphasized, and illustrated by the example
of blade-vortex interaction noise. The modification caused by surface
compliance of the efficiency of sound production by an adjacent flow i
s discussed by reference to simple analytical models involving vortex
flow near the edge of an elastic plate, and over a surface inhomogenei
ty on a large plate. (C) 1997 Published by Elsevier Science Ltd.