Aerodynamic measurement of a large aircraft model in hypersonic flow
Meng Bao-Qing1, 2, Han Gui-Lai1, †, Zhang De-Liang1, 2, Jiang Zong-Lin1, 2
       

(color online) (a) Experimental signals of the rods at tail; (b) compositions of CH9 signals (corresponding to the rod at tail).