Geometry Optimization of a Highly Integrated Flush Intake System Considering the Overall Aircraft
Year: 2025
Type: conference-paper
DOI: 10.2514/6.2025-3120
Institution: Universität der Bundeswehr München
Language: English
Subfield: Computational Mechanics
Field: Engineering
Domain: Physical Sciences
Open Access status: closed
OpenAlex ID: W4412485353
