Objectives

The discussion in the previous sections leads to the following two main objectives for the proposed research.

• Computational: Development of computational methods for the determination of aeroacoustical sound sources in low speed flows and methods to use these sources to compute the far field sound in all directions.

• Experimental: Development of an experimental setup for a jet flow at low speed with flow observation techniques that allow the validation of the computations of the aeroacoustical sound sources and with acoustical measurements that allow the verification of the radiated sound.