The original wing of the wooden training-glider SZD-9 "BOCIAN", of the Polish production, was modificated by using the additional carbon composite layer. The influence of the addition of a new carbon layer on the mechanical properties of the wing was investigated. Both objects were subjected to static loads, with measuring deflection lines and deformations of wing skin, and to dynamic loads. In dynamic investigations the vibration responses for broad-band excitations were determined as well as the frequencies of the resonance vibrations were tested. The effect of adding a carbon layer is strong damping of the dominant resonant frequency and reduction of the overall vibration level. This eff ectively makes it difficult to stimulate the construction for vibrations and therefore positively affects the safety of the wing.
Composite materials (fiber reinforced plastics, FRPs) are successfully utilized in the production of various mechanical devices, including land vehicles, marine vessels, and aircrafts. They are primarily used for the production of body parts and hulls. Due to their importance, certain requirements relating to the mechanical properties of the materials used must be met for such applications. One aspect of the passive safety of vehicles is the effects of a possible collision with another object. The behavior of the structure in such a case can be determined based on the coefficient of restitution, which is a measure of energy dissipation after an impact. This paper presents the results of measuring the value of the coefficient of restitution for the selected composite materials, utilizing various reinforcement materials including different types of fibers and wooden veneer. The selected materials included glass, carbon, Kevlar fibers, and veneer from exotic wood in an epoxy resin matrix. The tested samples were made using various methods in order to understand the influence of the technology on the value of the coefficient. The authors determined the coefficient values utilizing two methods based on the measurement of two different physical quantities. In the first case, the height of the rebound of the ram was measured using a fast digital camera; in the second case, the time between successive rebounds of the tool was measured, determined based on the signal from the acceleration sensor. The authors compared the results of the coefficient values obtained using these methods and examined the relationship between the rebound energy and the value of the coefficient of restitution. The results have been discussed, and some conclusions have been made. Among other things, it seems that both methods of measurement are interchangeable with regard to lower impact velocities corresponding to lower heights (up to 300 mm) of the drop of the ram used in the tests.
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