Wind Tunnel Testing of a Subsonic Airfoil Employing Hybrid Laminar Flow Control
Year: 2026
Type: article
Source: AIAA Journal
DOI: 10.2514/1.j065991
Institution: Technische Universität Braunschweig
Language: English
Subfield: Aerospace Engineering
Field: Engineering
Domain: Physical Sciences
Open Access status: closed
Funder: Deutsche Forschungsgemeinschaft
OpenAlex ID: W7161604375
