01 - Aircraft Design and Integrated Systems
FAST METHOD AND AN INTEGRATED CODE FOR SONIC BOOM PREDICTION OF SUPERSONIC COMMERCIAL AIRCRAFT
Y.-L. Ding¹, Z.-H. Han¹, J.-L. Qiao¹, W.-P. Song¹, B.-F. Song¹; ¹Northwestern Polytechnical University, China
This paper proposes an improved linear method for sonic boom prediction to promote its accuracy and robustness, by considering a suitable F-function and viscous effects. We develop the platform to predict sonic boom fast named FA-BOOM, which is able to make sonic boom prediction more accurate and effective in the next generation supersonic transports preliminary design.