In this work,a new method to solve the Reynolds equation including mass-conserving cavitation by using the physics informed neural networks(PINNs)is *** complementarity relationship between the pressure and the void f...
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In this work,a new method to solve the Reynolds equation including mass-conserving cavitation by using the physics informed neural networks(PINNs)is *** complementarity relationship between the pressure and the void fraction is *** are several difficulties in problem solving,and the solutions are ***,the difficulty for considering the pressure inequality constraint by PINNs is solved by transferring it into one equality constraint without introducing *** the void fraction inequality constraint is considered by using the hard constraint with the max-min ***,to avoid the fluctuation of the boundary value problems,the hard constraint method is also utilized to apply the boundary pressure values and the corresponding functions are ***,for avoiding the trivial solution the limitation for the mean value of the void fraction is *** results are validated against existing data,and both the incompressible and compressible lubricant are *** agreement can be found for both the domain and domain boundaries.
Re-ignited partially premixed flame(PPF)is a quite extensive flame type in real applications,which is directly relevant to the local and global extinction and re-ignition *** authors designed a model burner to establi...
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Re-ignited partially premixed flame(PPF)is a quite extensive flame type in real applications,which is directly relevant to the local and global extinction and re-ignition *** authors designed a model burner to establish laminar re-ignited *** simulations were carried out to reveal the morphology of laminar re-ignited *** on the distributions of temperature,heat release and radicals,the morphologies of re-ignited flames were explored.W-shaped flames were formed under pilot-lean ***-shaped and y-shaped flames were formed under pilot-rich *** w-shaped and y-shaped flames had a triple-flame *** re-ignited flames can stand beyond the rich flammability ***,OH distributions indicated both pilot flame and re-ignited flame well as it rapidly increased near the flame *** concentration did not increase visibly while CH2O concentration mildly increased during the mild re-ignition process in the pre-zone of the re-ignited *** to the results of 0-D simulations using closed homogeneous reactor,both OH and CH2O reduced ignition time *** results of this work are helpful for understanding re-ignited PPF more closely.
This paper proposes a novel self-calibration method for a large-FoV(Field-of-View)camera using a real star ***,based on the classic equisolid-angle projection model and polynomial distortion model,the inclination of t...
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This paper proposes a novel self-calibration method for a large-FoV(Field-of-View)camera using a real star ***,based on the classic equisolid-angle projection model and polynomial distortion model,the inclination of the optical axis is thoroughly considered with respect to the image plane,and a rigorous imaging model including 8 unknown intrinsic parameters is ***,the basic calibration equation based on star vector observations is ***,the partial derivative expressions of all 11 camera parameters for linearizing the calibration equation are deduced in detail,and an iterative solution using the least squares method is ***,simulation experiment is designed,results of which shows the new model has a better performance than the old *** last,three experiments were conducted at night in central China and 671 valid star images were *** results indicate that the new method obtains a mean magnitude of reprojection error of 0.251 pixels at a 120°FoV,which improves the calibration accuracy by 38.6%compared with the old calibration model(not considering the inclination of the optical axis).When the FoV drops below 20°,the mean magnitude of the reprojection error decreases to 0.15 pixels for both the new model and the old *** stars instead of manual control points are used,the new method can realize self-calibration,which might be significant for the long-duration navigation of vehicles in some unfamiliar or extreme environments,such as those of Mars or Earth’s moon.
In this study,a fingerprint analysis method along with the EEM fluorescence spectra was used to characterize the SAPs released by Scenedesmus ***1 during the growth *** fractionation was used firstly to divide the SAP...
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In this study,a fingerprint analysis method along with the EEM fluorescence spectra was used to characterize the SAPs released by Scenedesmus ***1 during the growth *** fractionation was used firstly to divide the SAPs into six resin fractions,and then size exclusion chromatography(SEC)was performed to separate each resin fraction into several subfractions with different molecular weights(MW).The fingerprint graph integrated the information revealed by resin fractionation as well as that by SEC,showing that main components of SAPs changed from the hydrophilic subfractions with MW of 10~2-10~3 Da to the hydrophobic subfractions with MW of 10~3-10~4 *** these results with the EEM fluorescence spectra of different resin fractions,the change of the main matters within SAPs could be inferred.
Linear rolling guideways(LRGs) play an important role in precision engineering. In the pre-rolling region, the hysteretic friction force exerts great impacts on the positioning accuracy. Numerical and experimental stu...
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Linear rolling guideways(LRGs) play an important role in precision engineering. In the pre-rolling region, the hysteretic friction force exerts great impacts on the positioning accuracy. Numerical and experimental studies of the hysteresis of friction force are presented in this paper. A model, which is based on the stripe theory and the simplified theory of rolling contact, is built to describe the transient hysteresis of the friction force. Then, the model is modified by taking the anelasticity effect into consideration. Experimentally, a linear motor direct-drive setup is utilized to measure the transient asymmetrical hysteresis of the friction force in the pre-rolling region of an LRG. The influences of the pre-rolling displacement and the dwelling time on the asymmetrical hysteresis of the friction force are studied. The numerical and experimental results are well correlated, which shows good accuracy of the model. The transient asymmetrical hysteresis of friction force in the pre-rolling region of LRGs can thus be determined using the model.
This paper presents a theoretical analysis of vibration control technology of wind turbine blades made of piezoelectric intelligent *** design of the blade structure,which is made from piezoelectric material,is approx...
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This paper presents a theoretical analysis of vibration control technology of wind turbine blades made of piezoelectric intelligent *** design of the blade structure,which is made from piezoelectric material,is approximately equivalent to a flat shell *** differential equations of piezoelectric shallow shells for vibration control are derived based on piezoelectric laminated shell *** this basis,wind turbine blades are simplified as elastic piezoelectric laminated *** establish the electromechanical coupling system dynamic model of intelligent structures and the dynamic equation of composite piezoelectric flat shell structures by analyzing simulations of active vibration *** results show that,under wind load,blade vibration is reduced upon applying the control voltage.
Numerical simulations are conducted to improve the energy acquisition efficiency of H-type vertical axis wind turbines through the optimization of the related blade airfoil aerodynamic *** Bézier curve is initi-ally u...
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Numerical simulations are conducted to improve the energy acquisition efficiency of H-type vertical axis wind turbines through the optimization of the related blade airfoil aerodynamic *** Bézier curve is initi-ally used tofit the curve profile of a NACA2412 airfoil,and the moving asymptote algorithm is then exploited to optimize the design of the considered H-type vertical-axis wind-turbine blade airfoil for a certain attack *** results show that the maximum lift coefficient of the optimized airfoil is 8.33%higher than that of the original *** maximum lift-to-drag ratio of the optimized airfoil exceeds the maximum lift-to-drag ratio of the ori-ginal airfoil by 11.22%.Moreover,the power coefficient is increased by 12.19%and the torque coefficient of the wind turbine is significantly improved.
Friction behaviors of linear rolling guides(LRGs)are determined by many factors and are crucial for precision *** is difficult to create an expression to describe the friction behaviors exactly and completely.A new ex...
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Friction behaviors of linear rolling guides(LRGs)are determined by many factors and are crucial for precision *** is difficult to create an expression to describe the friction behaviors exactly and completely.A new experimental method for measuring the friction behaviors of one LRG individually was developed,and linear motor direct drive technology is utilized in the experiment *** position signal is acquired by a grating,and the friction of the LRG is deduced by the product of the mass of the moving part and its *** the experiment,the LRG can move with the friction only,and the friction transition from normal rolling to prerolling stage was *** asperities’deformations were utilized to explain *** loops and internal loops were *** results indicate the non-local memory of the LRG,and the historical trajectory have an important impact on the friction behaviors of LRGs in the pre-rolling stage.
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