01.2 - Aircraft Design and Integrated System (Applications)
A RAPID DESIGN METHOD FOR QUIET SPIKE OF SUPERSONIC TRANSPORT AIRCRAFT
L.-W. Zhang¹, Z.-H. Han¹, J.-L. Qiao¹, Y.-L. Ding¹, Q. Chen¹, W.-P. Song¹; ¹Northwestern Polytechnical University, China
Aiming at reducing severe sonic boom raised by supersonic aircraft, this paper proposes a new design method of quiet spike. Compared with the traditional method, one can obtain a quiet spike shape rapidly by using this method, and it can be applied to engineering.