Advanced Design of a Transition Duct for Supersonic Inlet Turbines in Rotating Detonation Engines
Year: 2024
Type: article
Source: Journal of Turbomachinery
DOI: 10.1115/1.4067242
Authors: Noraiz Mushtaq, Matteo Pini, Paolo Gaetani
Institutions: Politecnico di Milano, Delft University of Technology
Language: English
Subfield: Aerospace Engineering
Field: Engineering
Domain: Physical Sciences
Open Access status: closed
OpenAlex ID: W4404587316