Abstract:

On the basis of the waverider configuration generated from the cone flow, the optimization design is conducted on the waverider forebody and the ramjet inlet. The design point (Ma=4.5) is the optimization basis for the waverider forebody, and the problem of the best flow turning angle under various flight Mach numbers is comprehensively taken into consideration. The numerical simulation results show that the waverider configuration designed by using this method conforms to the theory of waverider inverse designs and the ramjet inlet is of good performance in the whole range of flight Mach numbers.