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nr 2
EN
The article presents results of research on the micromorphology and anatomy of leaves of Morus alba cultivars. Mature leaves from generative shoots were collected in the Cytadela Park in Poznań and from trees planted along streets in different towns in the Wielkopolska region. A light microscope and a scanning electron microscope were used for observations. There were significant differences between the adaxial and abaxial epidermis. The idioblasts are found on the adaxial surface and stomata on the abaxial surface. Stomata can be classified into two types small and large. Several types of trichomes were recognized on the leaves: straight or hooked, unicellular, glandular capitate, spherical to elliptic stalked. Anatomical investigations revealed that leaves of M. alba cultivars were bifacial and the multi-layered mesophyll was diversified into palisade parenchyma and spongy palisade-like parenchyma. The research findings may be used for the identification of M. alba cultivars, while the epicuticular traits may be useful for the identification and classification of fragments of fossil leaves. The article includes descriptions and illustrations of several new quantitative and qualitative characters of the petiole and lamina, which have not been published previously and are described for the first time from Poland.
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tom R. 4, nr 12
439-443
PL
Koniecznym warunkiem do określenia własności fizycznych kompozytów wzmocnionych tkaniną modułową jest przeprowadzenie rozszerzonych badań, eksperymentalnych lub analitycznych. Ten pierwszy sposób, czyli badania eksperymentalne w przypadku ogromnej różnorodności dostępnych tkanin modułowych, osnów i struktur możliwych do otrzymania, stanowiłby bardzo duże nieekonomiczne przedsięwzięcie. Dlatego też najlepszym rozwiązaniem tego problemu jest stworzenie metody analitycznej, przewidującej własności fizyczne tych materiałów, co znacznie ograniczyłoby liczbę koniecznych badań eksperymentalnych. Praca ta przedstawia prymitywną teorię, opartą na nieco rozbudowanej teorii mieszanej dla kompozytów wzmocnionych tkaniną modułową. Określa stopień wiarygodności prostych wzorów, służących do oceny własności laminatów poprzez porównanie wyników teoretycznych z wynikami doświadczalnymi.
EN
Extensive studies are required to determinate values of material constants laminated composite plates with fabric reinforcement. The quantification can either be done experimentally or analytically. The innumerable diversity of woven fabrics, matrixes and potential combinations of the weave pattern in the fabric reinforced composites would make any experimental program very large and uneconomical. In this connection the best solution of this problem is to develop an analytical method to predict fabric composite behavior and validate the methodology through limited experimental studies. This validated analytical model can be used later to predict fabric composite behavior or to design fabric composites for a given set of conditions. In this work, a primitive theory has been shown, which is based on somewhat complicated theory for composites with fibre reinforcement. The purpose of this work is to study, in what degree the simple formulas, roughly estimating lamina properties, could be authenticated. This work consists of three parts. In the first part, composite model is presented (Fig. 1) that is considered as laminate consists of two unidirectional fibres-reinforced lamina. They are stacked that one lies crosswise against another and they can not displace between themselves. Unidirectional fibres are described by properties such as Young's modulus E(f), Poisson's rate v(f). Fibers are embedded in a isotropic matrix material described by properties such as Young's modulus E(0), Poisson's rate v(0). On the basis of this model, primitive theory is created, that makes the certain assumptions and restrictions, as stated here: perfect joint between layers, linearly elastic and orthotropic material of each layers, small strains and displacements, equal thickness of layers. At the end of part one author presents formulas of calculation Young's moduli of the laminate. Additionally author considers using the apparent Young's modulus of compressed fibre to calculating material constants of laminate. The second part includes formulas, that are used to determining shear module of laminate. Here analytical solutions are developed for optional computing elastic constants, which were present in the part one. In the last part comparison between theoretical and experimental measurements of material constants is presented (Tab. 1) to check effectiveness of present algorithm. Figures 1-3 show respectively laminate model, two cases of simple loading composite model by elementary force.
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