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- 저자 : Xianghua Jiang (검색결과 5 건)
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Jiang, Yunhe,Bao, Liang,Jeong, So‐,Yoon,Kim, Seong‐,Ki,Xu, Caiguo,Li, Xianghua,Zhang, Qifa Blackwell Publishing Ltd 2012 The Plant journal Vol.70 No.3
<P><B>Summary</B></P><P>Organ size is determined by cell number and size, and involves two fundamental processes: cell proliferation and cell expansion. Although several plant hormones are known to play critical roles in shaping organ size by regulating the cell cycle, it is not known whether brassinosteroids (BRs) are also involved in regulating cell division. Here we identified a rice T‐DNA insertion mutant for organ size, referred to as <I>xiao</I>, that displays dwarfism and erect leaves, typical BR‐related phenotypes, together with reduced seed setting. <I>XIAO</I> is predicted to encode an LRR kinase. The small stature of the <I>xiao</I> mutant resulted from reduced organ sizes due to decreased cell numbers resulting from reduced cell division rate, as supported by the observed co‐expression of <I>XIAO</I> with a number of genes involved in cell cycling. The <I>xiao</I> mutant displayed a tissue‐specific enhanced BR response and greatly reduced BR contents at the whole‐plant level. These results indicated that XIAO is a regulator of BR signaling and cell division. Thus, XIAO may provide a possible connection between BRs and cell‐cycle regulation in controlling organ growth.</P>
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Modeling of Microslip Friction and Its Application in the Analysis of Underplatform Damper
Luo Yangxiong,Jiang Xianghua,Wang Yanrong 한국항공우주학회 2018 International Journal of Aeronautical and Space Sc Vol.19 No.2
This paper presents a theoretical model for analyzing the damping effect of underplatform dampers for turbine blades. At first, tangential and normal contact stiffness of the friction damper were studied based on a flat-to-flat contact model. The analyticexpressionsofcontactstiffnesswerepresented.Then,amicroslipmodelwasdeveloped,andthefrictionalhysteresis loops were obtained by the Masing hypothesis. The so-called “B–B” (Blade to Blade) model was studied in this paper, and both cylindrical and wedge-shaped dampers were calculated in the case studied. The inertia and rotating effect of the damper were ignored for simplicity. Thus, the damper’s motion between blade platformlocations could be determined by iteration of forcebalanceequationsofthedamperoncetheblades’motionsasinputsofthesystemweredetermined.Theeffectofnormal load on the contact stiffness was ignored for simplicity. The friction force was linearized by harmonic balanced method, considering only the first-order harmonic terms. Finally, the relationship between damping ratio and the maximum vibration stress of the blades was calculated to assess the damping effect of the damper.
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Effect of Front and Rear Rotor Stages on Aeroelasticity in Multi-Stage Environment
Xiaobo Zhang,Yanrong Wang,Xianghua Jiang,Zhizhong Fu 한국항공우주학회 2019 International Journal of Aeronautical and Space Sc Vol.20 No.1
An energy method based on the mixing-plane model and phase lagged boundary condition has been developed to estimate the flutter characteristics of rotor blades in multi-stage environment. The effects of front and rear rotor stages on the aerodynamic damping of the rotor blades have been investigated using this method. The results show that the mixing-plane model enables to consider the averaging effect of the other stages on the aeroelasticity of the checked rotor blades without having to perform the unsteady full annual multi-stage (FAMS) flow computations. Comparing with the isolated rotor blade, the upstream and downstream rotor stages have a significant influence on the aeroelasticity of the rotor blade with altering the intensity and location of the shock wave and separation flow region on suction surface. It is worth to point out that the neighbor rotor stages reduce the effect of the inter-blade phase angle (IBPA) on the aerodynamic damping. Moreover, the impact of the rear rotor stage on aerodynamic damping of the rotor blade is more remarkable than that of the front one. Compared to the measured data, the capability of this method used in the aeroelasticity assessment of a multi-stage turbomachine has been validated. Furthermore, the relationship between the aerodynamic damping and the motion of the shock wave has been revealed, which can assist the compressor design.
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Effects of Montmorillonite Nanocomposite on Mercury Residues in Growing/Finishing Pigs
Lin, Xianglin,Xu, Zirong,Zou, Xiaoting,Wang, Feng,Yan, Xianghua,Jiang, Junfang Asian Australasian Association of Animal Productio 2004 Animal Bioscience Vol.17 No.10
The study was conducted to evaluate the effects of montmorillonite anocomposite (MNC) on mercury residues in growing/finishing pigs. A total of 96 cross bred pigs ($Duroc{\times}Landrace{\times}large$ white, 48 barrows and gilts respectively), with similar initial weight (27.87${\pm}$1.15 kg), were used in this study. The animals were randomly assigned to two concentrations of mercury (0.1 and 0.3 ppm from $HgCl_2$) and two levels (0 and 0.3%) of MNC in a $2{\times}2$factorial arrangement of treatments. Each group has 3 pens (replications), and each pen has 8 pigs (4 barrows and 4 gilts). The experiment lasted for 90 days. The results showed that pig growth performances were not affected significantly by inclusion of Hg and addition of MNC (p$\geq$0.05). It indicated that the extent of intoxication in these pigs were not severe enough to impair growth performances. Both on the bases of 0.1 ppm and 0.3 ppm mercury supplementations, addition of 0.3% MNC markedly decreased mercury levels of blood, muscle, kidney and liver tissue (p<0.05). These results implied that the addition of non-nutritive sorptive material, MNC, could effectively reduce the gastrointestinal absorption of mercury via its specific adsorption, with a consequent reduction of mercury residues in body tissues. MNC had offered an encouraging solution to produce safe animal products with mercury contaminated feed.
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