Numerical simulation of sonic boom near-field flow over C25D model.

The results of numerical simulation of sonic boom near field flow around the NASA Concept 25D (C25D) low-boom supersonic demonstrator configuration are presented. The calculations were carried out for a stationary flow of an ideal gas in a three-dimensional mode with a help of SOLIDWORKS Flow Simulation solver. Comparison with the results of numerical simulations obtained by researchers in the framework of the 2nd AIAA Sonic Boom Prediction Workshop is made. [ABSTRACT FROM AUTHOR]