03.4 - Applied Aerodynamics
SONIC BOOM ANALYSIS OF DIFFERENT SUPERSONIC AIRCRAFT
A. Glorioso¹, F. Petrosino², M. Barbarino², G. Pezzella¹, A. Viviani¹; ¹University of Campania, Italy ;²CIRA, Italy
The focus of this work is to evaluate and compare the sonic boom of three different supersonic aircraft concepts, developed in the European project MORE&LESS, through a numerical approach. Aerodynamic simulations were performed using the open-source solver SU2, while noise propagation from the aircraft to the ground was evaluated using an in-house code developed at Hamburg University TUHH.