Typical Mixing Enhancement Approaches in Supersonic Crossflow

Scramjet refers to air entering the combustion chamber at supersonic speed and then mixing and burning with fuel. However, in the condition of such a fast flow speed, it is difficult to achieve full mixing and stable combustion of fuel and air. The previous condition of stable combustion is the full...

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Bibliographic Details
Main Author: Zhou Yanmei, Wu Jiping, Huang Wei
Format: Article
Language:zho
Published: Editorial Office of Aero Weaponry 2023-04-01
Series:Hangkong bingqi
Subjects:
Online Access:https://www.aeroweaponry.avic.com/fileup/1673-5048/PDF/2022-00261.pdf