Modal Test and Finite Element Model Update of Aircraft with High Aspect Ratio Wings
نویسندگان
چکیده
منابع مشابه
Nonlinear Aeroelastic Analysis of Aircraft with High-aspect-ratio Wings
The paper describes a formulation for aeroelastic analysis of aircraft with high-aspect-ratio wings. The analysis is a combination of a geometrically-exact mixed formulation for dynamics of moving beams and finite-state unsteady aerodynamics with the ability to model dynamic stall. The analysis also takes into account gravitational forces, propulsive forces and rigidbody dynamics. The code has ...
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ژورنال
عنوان ژورنال: Transactions of the Korean Society for Noise and Vibration Engineering
سال: 2012
ISSN: 1598-2785
DOI: 10.5050/ksnve.2012.22.5.480