Virtual Full Scale Static Test of a Civil Tilt Rotor Composite Wing in Non-Linear Regime.
- Resource Type
- Article
- Source
- Aerospace (MDPI Publishing); Apr2024, Vol. 11 Issue 4, p278, 19p
- Subject
AIRPLANE wings STRAINS & stresses (Mechanics) STRUCTURAL failures TILT-table test STRESS concentration STRUCTURAL design ROTORS - Language
- ISSN
- 22264310