Advances in computational aeroacoustics (CAA) depend critically on the avai
lability of accurate, nondispersive, least dissipative computation algorith
m as well as high-quality numerical boundary treatments. This paper focuses
on the recent developments of numerical boundary conditions. In a typical
CAA problem, one often encounters two types of boundaries. Because a finite
computation domain is used, there are external boundaries. On the external
boundaries, boundary conditions simulating the solution outside the comput
ation domain are to be imposed. Inside the computation domain, there may be
internal boundaries. On these internal boundaries, boundary conditions sim
ulating the presence of an object or surface with specific acoustic charact
eristics are to be applied. Numerical boundary conditions, both external or
internal, developed for simple model problems are reviewed and examined. N
umerical boundary conditions for real aeroacoustic problems are also discus
sed through specific examples. The paper concludes with a description of so
me of the much-needed research in numerical boundary conditions for CAA.