Modal decomposition of the unsteady non-reactive flow field in a swirl-stabilized combustor operated by a Lean Premixed injection system
Year: 2021
Type: article
Source: Aerospace Science and Technology
Institution: Universitat Politècnica de València
Language: English
Subfield: Computational Mechanics
Field: Engineering
Domain: Physical Sciences
Open Access status: bronze
Awards: G3040591464, G4542525632
OpenAlex ID: W3134441010