Abstract: This paper discusses the design process of computational codes of jet noise semi-empirical prediction method based on TA model. In this work, the flow field is simulated by ANSYS Software, such as ICEM and FLUENT. The sound pressure level is calculated by Fortran90 codes. The results of the computation codes agree well with the experiment data of Tam. We also refer to a simplification method to cut down the CPU time and satisfy the accuracy as well.