This paper reviews important advances in understanding and predicting
the behavior of scramjet combustion systems since the classic article
published in this series by Antonio Ferri (1973). The review focuses o
n basic fluid phenomena and is divided into three distinct sections. T
he first briefly describes progress that has been made in the design a
nd demonstration of practical scramjets around the world, especially i
n the US, the FSU, France, and Germany. The second provides a contempo
rary exposition of the aerothermodynamics of the dual-mode ramjet/scra
mjet combustion system, accounting for the role of the isolator in pre
venting unstart from either thermal choking or how separation due to h
eat release. The third part summarizes the current state of knowledge
regarding fuel-air mixing in dual-mode ramjet/scramjet combustors, esp
ecially the potential of axial vorticity to increase mixing effectiven
ess over that of lateral vorticity.