Work

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
Open Access status: gold
Estimated APC paid: $1,000
OpenAlex ID: W4408804650
FWCI: 1.377
Cites:
Cited by: 3
Related to: 10