Work

A parametric three-dimensional study of combustion modes and thrust performance in rotating detonation engine with aerospike nozzle

Year: 2025

Type: article

Source: Physics of Fluids

DOI: 10.1063/5.0256511

Authors: Yang Wang, Shuzhen Niu, Zixi Zhao, Wenqiang Du, Cheng Tian

Institutions: Beijing Institute of Technology, Peking University, State Key Laboratory of Turbulence and Complex Systems, Tsinghua University

Language: English

Topic: Combustion and Detonation Processes

Subfield: Aerospace Engineering

Field: Engineering

Domain: Physical Sciences

Open Access status: closed

Funder: National Natural Science Foundation of China

Awards: G1202390635, G52471181

OpenAlex ID: W4408575035

FWCI: 2.398

Cites: 37

Cited by: 6

Related to: 10