33 research outputs found

    A Zero-placement Technique for Designing Shaped Inputs to Suppress Multiple-mode Vibration

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    than traditionally designed shapers of comparable duration. Computer simulations of a single-mode system demonstrated the advantages of the new shapers. MACE results collected aboard the Space Shuttle Endeavor demonstrated the shapers' vibration-reducing abiUty on real structures. Acknowledgments W

    Shaped Input Control of a System With Multiple Modes

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    Wytrzyma艂o艣膰 na 艣cieranie prz臋dz krzy偶uj膮cych si臋 pod k膮tem prostym

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    This paper investigates yarn abrasion behaviour based on the yarn structure, twist factor and fibre alignment at the rubbing contact points (twist direction at contact points). First yarns arranged at right angle (utilized with a high resolution camera) were introduced on a yarn abrasion tester and then the abrasion behaviour of the ring (R) and open-end rotor (O.E.) spun yarns were compared and analysed. Comparison of the yarns indicates that the abrasion resistance thereof is affected by the twist factor in a way that as the twist increases, the yarn on yarn abrasion cycles to failure follows the same trend as the effect of twist on the yarn strength (first an increase and then a decrease); that is, yarn on yarn abrasion resistance increases up to a certain degree (a=140 in ring spun yarn and a=156 in open-end rotor spun yarn), and then as the twist increases, the yarn on yarn abrasion resistance decreases. It also shows that the yarn abrasion cycle to failure is lower when the fibre alignments of the contact yarns are in the same direction. Close observation of the yarn rubbing also indicates that as the fibres are removed from the outer layers, the rotor spun yarn shows higher yarn on yarn abrasion resistance; that is, moving from the outer side to the interlayer of the rotor spun yarn, the relative yarn on yarn abrasion resistance (abrasion cycles to failure/yarn count) increases. This phenomenon indicates the fact that in open-end rotor spun yarn the compactness of the interlayer fibres are higher than the compactness of the outer layer fibres.Analizowano r贸偶ne w艂a艣ciwo艣ci mechaniczne przy zrywaniu lnianych prz臋dz 艂膮czonych r贸偶nymi w臋z艂ami, stosuj膮c test na rozci膮ganie dla czterech w臋z艂贸w o r贸偶nej strukturze - w臋ze艂 prosty, zwyk艂y, tkacki i rybacki. Zastosowano cztery pr贸bki: 50 tex (A - bielona, B - surowa) i 68 tex (C - bielona, D - surowa), ka偶da wyprz臋dziona z lnu. W pracy przedstawiono warto艣ci si艂y zrywaj膮cej, wytrzyma艂o艣ci przy zerwaniu, wyd艂u偶enia przy zerwaniu, pracy do zerwania oraz jednostkowej pracy do zerwania dla prz臋dz 艂膮czonych w臋z艂ami. Ponadto, przeanalizowano wsp贸艂czynnik retencji dla si艂y zrywaj膮cej, wyd艂u偶enia przy zerwaniu i pracy przy zerwaniu. Stwierdzono, 偶e wytrzyma艂o艣膰 prz臋dz 艂膮czonych w臋z艂ami zale偶y w du偶ym stopniu od struktury w臋z艂贸w, podczas gdy prz臋dze surowe i bielone wykaza艂y podobne w艂a艣ciwo艣ci wytrzyma艂o艣ciowe

    Mechanical Modeling of Fabrics in Bending

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    Vibration of a Rotating Timoshenko Beam

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    Geometric Stiffening of Timoshenko Beams

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    The Simplest Plate Bending Finite Element

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