Influence of oncoming flow parameters on rotating detonation combustor with supersonic turbine guide vanes

• Main Authors: Wen, Fengbo, Su, Liangjun, Wang, Ying, Han, Jiajun, Wang, Songtao
• Other Authors: School of Mechanical and Aerospace Engineering
• Format: Article
• Language: English
• Published: 2024
• Subjects: Engineering; Detonation waves; Flow parameters
• Online Access: https://hdl.handle.net/10356/178346
• Institution: Nanyang Technological University

Rotating detonation combustion can greatly improve the performance of air-breathing turbojet engines due to its self-pressurization and high combustion efficiency. Detonation wave propagation is closely related to oncoming flow parameters. The supersonic turbine guide vane plays a role in weakening...