Numerical Investigation of Two-Phase n -Decane/Air Rotating Detonation Engines With Different Numbers of Fuel Orifices
Year: 2024
Type: article
DOI: 10.1115/1.4066607
Institution: Harbin Engineering University
Language: English
Subfield: Aerospace Engineering
Field: Engineering
Domain: Physical Sciences
Open Access status: closed
OpenAlex ID: W4402859499
