Design and Optimization Method for Scaled Equivalent Model of T-Tail Configuration Structural Dynamics Simulating Fuselage Stiffness
Release Time:2026-03-18 Hits:
Indexed by: Journal Papers
Document Code: 595819
Date of Publication: 2025-11-30
Journal: AEROSPACE
Volume: 12
Issue: 12
Key Words: NATURAL FREQUENCIES; TRUSS STRUCTURES