Two patent documents that are related to the high-supersonic aircraft currently discussed above, titled "一种用于高马赫飞机的可变倾角尾翼构型" ("A variable-incidence tail configuration for high‑Mach aircraft") and "一种压燃冲压发动机进发排匹配设计方法" ("
A design method for matching the inlet, engine, and exhaust of a compression‑ignition ramjet"). Note that both documents share three authors and were filed last month. Posted by @一定会对蛙动手 on Weibo.


A design method for matching the inlet, engine, and exhaust of a compression‑ignition ramjet"). Note that both documents share three authors and were filed last month. Posted by @一定会对蛙动手 on Weibo.

