Numerical Study of a UAV with Tandem Wing under Gust Load Influence using Two-Way Fluid-Structure Interaction Method
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
Authors
- Mahesa Akbar (ORCID: https://orcid.org/0000-0001-7998-0846)
- Mochammad Agoes Moelyadi (ORCID: https://orcid.org/0000-0001-8740-6959)
- David Waldo Parlindungan
Publication Details
- Journal
- International Journal of Technology
- Published
- 2025-03-25
- DOI
- https://doi.org/10.14716/ijtech.v16i2.6289
- Citations
- 1
- Primary Topic
- Biomimetic flight and propulsion mechanisms
- Type
- article
- Field-Weighted Citation Impact
- 4.99