Wave computation in compressible flow using space-time conservation element and solution element method

The recently developed space-time conservation element solution element met hod has several attractive features for aeroacoustic computations. The sche me is robust, possesses almost no dispersion error, and the implementation of nonreflecting boundary conditions is simple and effective. The scheme is tested for several problems ranging from linear acoustic waves to strongly nonlinear phenomena, with special emphasis on mixing-layer instability, an d good numerical results are achieved.