Author:
Kovalovs Andrejs,Chate Andris,Kulakov Vladimir,Mironov Aleksey
Abstract
This paper presents a comparative investigation of the effect of hand lay-up to manufacture of composite structure on the elastic constants of composite cylindrical shells. Non-destructive technique for detection of elastic constants in laminated composite cylinders were applied. This technique based on numerical-experimental method that included experimental testing and numerical modelling. Experimental testing includes determination of natural frequencies in composite cylinders fixed at the ends. Composite construction fixed by upper end on the special test bench to realize clamped-free boundary conditions. 48 piezo sensors were glued on the outer surface of composite shells to measure strains during testing. Data received during experiments were converted in modal parameters using ARTEMIS software. By minimizing the error functional between the numerical and experimental data of the natural frequencies, the properties of laminated composite materials were obtained. It can be seen that elastic constants of the five composite shells have insignificant differences in values and be successfully applied for numerical calculation in further.
Reference25 articles.
1. Weight optimal design of lateral wing upper covers made of composite materials
2. Optimal design of composite lateral wing upper covers. Part II: Nonlinear buckling analysis
3. Modeling and Design of a Full-Scale Rotor Blade with Embedded Piezocomposite Actuators
4. Masarati P., Morandini M., Riemenschneider J., Wierach P., Gluhih S. and Barkanov E. “Optimal Design of an Active Twist 1:2.5 Scale Rotor Blade,” in 31st European Rotorcraft Forum 2005, Proceedings of the 31st European Rotorcraft Forum (Curran Associates publishing, Red Hook, NY, 2010), pp. 37.1-37.14.