Numerical Study of the Effects of Injection Conditions on Rotating Detonation Engine Propulsive Performance

Numerical Study of the Effects of Injection Conditions on Rotating Detonation Engine Propulsive Performance

A three-dimensional upwind conservation element and solution element method (CESE) in cylindrical coordinates is first developed to effectively solve the unsteady reactive Euler equations governing a hydrogen–air rotating detonation engine (RDE) with coaxial structures. The effects of the annular wi...

Full description

Bibliographic Details
Main Authors: Lisong Shi, E Fan, Hua Shen, Chih-Yung Wen, Shuai Shang, Hongbo Hu
Format: Article
Language:English
Published: MDPI AG 2023-10-01
Series:Aerospace
Subjects:
rotating detonation
numerical simulation
three-dimensional effect
propulsion performance
CESE method
Online Access:https://www.mdpi.com/2226-4310/10/10/879

Internet

https://www.mdpi.com/2226-4310/10/10/879

Similar Items