Numerical Study of a UAV with Tandem Wing under Gust Load Influence using Two-Way Fluid-Structure Interaction Method
Year: 2025
Type: article
Abstract: This paper presents a new investigation of a tandem wing configuration under cruise and gust load conditions. A wing of a high-altitude long-endurance unmanned air vehicle (HALE UAV) is used as a case study. A two-way fluid-structure interaction (FSI
Language: English
Subfield: Computational Mechanics
Field: Engineering
Domain: Physical Sciences
Open Access status: gold
Estimated APC paid: $1,000
OpenAlex ID: W4408804650
