Design Optimization of Rear-Fuselage Boundary-Layer Ingestion Shrouded Propulsor
Year: 2025
Type: article
Source: Journal of Aircraft
DOI: 10.2514/1.c038084
Institutions: HIT09 (Italy), University of Padua
Language: English
Subfield: Global and Planetary Change
Field: Environmental Science
Domain: Physical Sciences
Open Access status: closed
Funder: Cleansky
Award: G4929230081
OpenAlex ID: W4407317643
