Analysis of Aerodynamic Characteristics of Rotating Detonation Turbine Based on Proper Orthogonal Decomposition Method

The unsteady interactions in rotating detonation turbine engines (RDTE) remain poorly understood. To address this, a 2D numerical model integrating a rotating detonation combustor (RDC) with a first-stage turbine is established to analyze flow structures and aerodynamics under various detonation mod...

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Detalhes bibliográficos

Principais autores:	Meiting Ling, Ting Zhao, Wenguo Luo, Jianfeng Zhu, Yancheng You
Formato:	Artigo
Idioma:	Inglês
Publicado em:	MDPI AG 2025-05-01
Colecção:	Aerospace
Assuntos:	rotating detonation turbine engine detonation wave propagation mode turbine aerodynamic characteristics POD
Acesso em linha:	https://www.mdpi.com/2226-4310/12/5/406
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