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    2025,23(2):1-9, DOI: 10.6052/1672-6553-2024-080
    Abstract:
    To enhance the isolation performance of the current three-parameter isolators, a prototype of broadband fluid damping strut has been designed. The damping strut features several frequency selective valves to adjust its damping characteristics at the low-frequency range, and a machined spring with a clearance element to act as a secondary stiffness. A dynamic mathematical model and a simulation model of a vibration isolation system using the designed fluid damping strut for a spacecraft control moment gyroscope have been established, followed simulation results indicate that compared to current three-parameter dampers the designed damping strut has achieved adaptive outer characteristics of high damping in the low-frequency range and low damping in the high-frequency range, it has obtained a significant suppressive effect on low-frequency vibrations, especially those near the resonance peak, its statistical vibration isolation effect is also better than that of the current dampers in the mid and high frequency bands, thus, the designed fluid damping strut has obtained excellent vibration isolation characteristics in a broad frequency band.
    2025,23(2):10-16, DOI: 10.6052/1672-6553-2024-066
    Abstract:
    Most of the current research methods use the prediction correction method, but other numerical methods are less frequently used. In this paper, a numerical method for computing fractional-order dynamical systems is elaborated using Lagrange polynomial interpolation. And this is used to successfully obtain an effective numerical solution for a new fractional-order jerk chaotic system. The results obtained are compared with those of the prediction correction method and found to be in good agreement with each other, verifying the validity of this method. The maximum Lyapunov exponent of the new fractional-order jerk chaotic system is further explored for different system orders, and it is concluded that the system exhibits instability when the system order α=0.85, α=0.95, and the phase diagram of the system in Caputo’s sense is further demonstrated.The results show that different system order α have a significant effect on the dynamical behaviour of new fractional order jerk chaotic system.
    2025,23(2):17-22, DOI: 10.6052/1672-6553-2024-065
    Abstract:
    On the basis of the two-component coupled Hirota equation, the higher-order solitons solution of the equation is investigated, and dynamical characteristics is analyzed. Based on the Lax pair and generalized Darboux transformation, the Taylor expansion of the characteristic function is carried out, and the expressions of the second-order and third-order soliton solutions of Hirota equation are derived. The real and imaginary parts of spectral parameter λ are discussed in different cases. Under the influence of the value of different free parameters, the evolution graphs of soliton interaction are obtained via numerical simulation. The effects of different parameters on the amplitude change and propagation direction of solitons are analyzed. The results show that different values of parameters affect the interaction and propagation direction of solitons.
    2025,23(2):23-29, DOI: 10.6052/1672-6553-2024-070
    Abstract:
    For vibration and noise reduction of the most railway wheels, corresponding dampers are generally installed to increase the structural damping of wheels, so as to reduce vibration and noise. Wheel-damper system was a wheel system with multilayer damper installed. The dynamic model of wheel-damper system of railway vehicle was established, and the equivalent ratio model of wheel-damper system was derived. A method for obtaining the modal damping ratio of structures based on theoretical model and simulation and independent of modal test was presented. Combined with abaqus modal superposition method, the vibration frequency response function(FRF) of the wheel-damper system was calculated. Finally, the vibration frequency response function of the wheel-damper system was tested, and the simulation results are in good agreement with the text results, which shows that the method is an important means to qualitatively compare the damping performance of different wheel damper devices in the design stage.
    2025,23(2):30-37, DOI: 10.6052/1672-6553-2024-076
    Abstract:
    This study proposes a ROV-based deep-sea mining system to overcome the stability issues of tracked vehicles in the traditional deep-sea mining system. The ROV-based deep-sea mining vehicle replaces the traditional tracked deep-sea mining vehicle. The ROV-based deep-sea mining vehicle consists of a remote operated vehicle (ROV) and a mining robot (MRT). First, this paper investigates the dynamic model of the ROV-based mining vehicle, assuming that the ROV maintains a fixed depth while towing the MRT. By analogy with a bicycle model, the dynamic model of the ROV-based mining vehicle is established. Subsequently, a hierarchical path tracking control strategy is introduced. Based on the kinematic model of the ROV-type mining vehicle, a linear model predictive control (LMPC) controller is designed to calculate a virtual control law for converging MRT path tracking deviations. A lower-level PID controller computes the ROV control input in response to the virtual control law. Finally, the feasibility of the hierarchical path tracking control strategy is preliminarily validated through numerical simulations.
    2025,23(2):38-46, DOI: 10.6052/1672-6553-2024-088
    Abstract:
    As the deployment of low-orbit large constellations reaching its peak with rapidly expanding scales, this study investigates the internal collision risks during the deployment of large low-Earth orbit (LEO) satellite constellations. A constructed constellation is used as an example to analyze the effect of phase parameters and orbital inclination on internal collision risk. Two methods are employed: the spherical geometry method, which does not consider perturbation effects, and the collision probability method, which does consider perturbation effects, to calculate the constellation's minimum distance and collision probability. Collision analysis reveals that the overall minimum distances decrease when perturbations are considered. Moreover, consistency is observed between the optimal configurations for minimum distance and collision probability indices when perturbations are taken into account. The study also discovers that the minimum distances of the constellation fluctuate periodically by 2° to 6° as orbital inclination increases. Based on these findings, an optimization strategy is proposed that involves fine-tuning the orbital inclination to reduce collision risks. Additionally, a configuration design strategy is designed to improve the computation precision with limited computational resources, namely the “initial screening of inclination by geometric method followed by detailed phase parameter screening with perturbation”
    2025,23(2):47-54, DOI: 10.6052/1672-6553-2024-071
    Abstract:
    Aiming at the problem of fuel-optimal control of hypersonic vehicles (HSV) in the ascending stage, a trigonometric regularization method is introduced based on the optimal control indirect method. This method makes up for the shortcoming of the indirect method: The derivation of the first-order optimal necessary condition for complex optimal control problems is cumbersome, singular optimal problem is difficult to solve and the optimal control is unsmooth. Aiming at the problem of divergence due to the improper initial costate variables guess in the two-point boundary value problem(TPBVP) transformed the indirect method, the continuation method is introduced and improved. The method uses the solution of the simplified problem as the initial value of the continuation, and through solving a series of TPBVP, approximates to the solution of the original problems. The simulation results show that through the above methods, the fuel-optimal control problem of HSV in the ascending stage under the complex model can be solved reliably.
    2025,23(2):55-63, DOI: 10.6052/1672-6553-2024-058
    Abstract:
    Dynamic models serve as effective tools for simulating physical systems, facilitating a deeper understanding of the operational principles governing systems. They provide theoretical underpinnings for prediction, optimization, and control system development. In recent years, data-driven approaches for dynamic modeling have garnered widespread attention in academia. While significant progress has been made, there remain limitations. This paper delves into the data-driven modeling of planar articulated multibody systems and proposes an improved neural network framework, termed Topological Lagrangian Neural Network (TLNN), building upon the foundation of Lagrangian Neural Networks (LNN). Compared to LNN, TLNN leverages topological information embedded within multibody systems, enhancing the learning performance of neural networks. Prediction results demonstrate that TLNN establishes higher-precision dynamic proxy models for articulated multibody dynamics compared to LNN, Hamiltonian Neural Networks (HNN), and Neural Ordinary Differential Equations (NODE) when trained on the same dataset. Furthermore, this paper discusses the generalized coordinate selection issue in the data-driven modeling process. Both training and prediction results indicate that utilizing rigid body absolute angles for modeling yields dynamic proxy models with higher precision compared to modeling based on joint relative angles in data-driven modeling of articulated multibody systems.
    2025,23(2):64-71, DOI: 10.6052/1672-6553-2024-061
    Abstract:
    The phenomenon of vibrational resonance holds significant application value in weak signal detection and energy harvesting. However, existing studies predominantly focus on symmetric bistable systems or linear dissipation scenarios. To address this gap, this paper investigates vibrational resonance (VR) in an asymmetric bistable system with nonlinear dissipation,driven by biharmonic forces at two different frequencies. The fast and slow variable separation method is applied to derive the response amplitude of the system at low frequencies. Moreover,based on the analytical expression of the response amplitude,the effects of the dual-frequency periodic signal,the nonlinear dissipation and the asymmetric parameter on the VR are investigated. The results indicate that,first,the larger the nonlinear dissipation factor,the weaker the VR of the system occurs. Second,for the systems with nonlinear dissipative term,tuning the asymmetric parameter can change the shape of the VR,that is,the symmetric bistable systems emerge the double resonance,and the asymmetric bistable systems have the single resonance. Third,the asymmetric parameter does not influence the location of the VR,but it can weaken the response amplitude. Finally,the theoretical predictions are in good agreement with the numerical simulation results,verifying the validity of the theoretical analysis.
    2025,23(2):72-82, DOI: 10.6052/1672-6553-2024-050
    Abstract:
    Gap junctions play an important role in the transmission of information between neurons, the development of neural circuits, and the understanding of the working mechanism of the nervous system. The direct coupling between neurons connected by gap junctions may contribute to the synchronization of neuronal firing and the emergence of sharp wave-ripples(SWR), which affect brain functions such as memory consolidation. Because gap junctions are so few in the mature brain, they have been ignored in earlier studies. Considering the heterogeneous characteristics of excitatory and inhibitory neurons, it is unclear whether gap junctions in different neuronal types can provide a corresponding compensatory mechanism for SWR in abnormal networks. In order to explore the above problems, a network of neurons in CA1 region of hippocampus with introduction of gap junctions was constructed, which consisted pyramidal cells, parvalbumin-positive basket cells, and axon-axonic cells. The results show that when the chemical synapses in CA1 are weakened and cannot generate SWR synchronous discharge, gap junctions in pyramidal cells and parvalbumin-positive basket cells can promote SWR. The SWR compensation was most effective when gap junctions in pyramidal neurons and in both types of neurons were present.
    2025,23(2):83-92, DOI: 10.6052/1672-6553-2024-018
    Abstract:
    Appling pre-defined-time stability theory, three controllers were designed to achieve synchronization between Chen-Qi-like four-dimension hyper-chaotic driving systems and response systems of the same type with unknown parameters within a pre-defined time based on tangent function, hyperbolic tangent function, or exponential function. Theoretical proofs were provided. Its’effectiveness were testified with state time history diagrams and synchronous error curves via numerical simulation. The results indicated that controllers designed can achieve to synchronize to chaotic motion while the driving system in chaotic motion, and with a small convergence time difference among the four state synchronization errors. But there was a significant convergence time difference in the four state synchronization errors while driving system in periodic motion. That was induced by the imbalance and mismatch of the state cubic nonlinear term essentially. The results also indicated that adaptive controller and parameter correction law based on tangent function had a larger range of adaptability to initial state values and system parameters comparing to the other two controllers and parameter adaptive laws, thus it hold a better universality.
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    2014,12(3):269-273, DOI: 10.6052/1672-6553-2014-043
    [Abstract] (3373) [HTML] (0) [PDF 336.30 K] (21581)
    Abstract:
    Aiming at the problem that the longitudinal modes of structural system of rocket need to be identified from its integral modes in engineering, a method that automatically identifies the longitudinal modes of structural system of rocket was proposed according to the theory of modal effective mass. Taking the vibration characteristics of system with lumped mass as a computing example, applying the finite element software, the beam model of system with lumped mass was established, and the longitudinal modes of the system were automatically identified based on the method. Compared with the system modal information calculated by the method of modal analysis, this automatic identification method not only can accurately identify the longitudinal modes of vibrating system, but also has automatic and high efficiency identification feature. It provides a theoretical basis for the dynamic model of POGO vibrating system in liquid rockets and other model of engineering systems to be accurately and promptly established.
    2014,12(3):193-200, DOI: 10.6052/1672-6553-2014-046
    [Abstract] (3189) [HTML] (0) [PDF 748.46 K] (18995)
    Abstract:
    The spacecraft's ability to adapt to the harsh dynamics environment is critical for the whole space mission. Vibration test control technology is the key part of the dynamic environment test. The current progress, fundamental principles and key techniques development level of the spacecraft and vibration control algorithms overseas were analyzed. The basic ideas, effective ways and suggestions were given to domestic following research.
    2017,15(5):385-405, DOI: 10.6052/1672-6553-2017-039
    [Abstract] (2007) [HTML] (0) [PDF 1.91 M] (18842)
    Abstract:
    In this review article, the growth and related academic communications in the dynamics of multibody systems are firstly surveyed. Then, the recent advances in the numerical algorithms for solving the dynamic equations of flexible multibody systems, the contact/impact dynamics of flexible multibody systems and the deployment of flexible space structures are systematically reviewed, together with several open problems of concern. Finally, some suggestions are made for the prospective researches on the dynamics of flexible multibody systems.
    2014,12(1):18-23, DOI: 10.6052/1672-6553-2013-068
    [Abstract] (3107) [HTML] (0) [PDF 1.13 M] (18540)
    Abstract:
    The electromechanical coupling model of cantilevered piezoelectric harvester was developed by considering the nonlinearities of piezoelectric material, based on Hamilton theory, Rayleigh-Ritz method, Euler-Bernoulli beam theory and constant electrical field across the piezoelectric element. The response characteristics of the system were investigated numerically, and the influences of piezoelectric material nonlinear coefficient on the system response were analyzed. By exploring the nonlinear characteristics of the piezoelectric vibrator near the resonant frequency, the nature of the multi-solutions and jump phenomena in the resonance region was revealed. The results were verified experimentally. which provides a theoretical basis for the study of nonlinear mechanism of piezoelectric power generation system.
    2014,12(3):243-247, DOI: 10.6052/1672-6553-2014-054
    [Abstract] (2513) [HTML] (0) [PDF 1.07 M] (18115)
    Abstract:
    Random vibration test is very important to the aerospace equipment. The windage of ASD outside the frequency bandwidth was analyzed. The reason, premonition, affection and effective way were given. And the commonly used random vibration test and vibration test metrology standard for the ASD outside the frequency bandwidth were analyzed.
    2016,14(2):97-108, DOI: 10.6052/1672-6553-2015-009
    [Abstract] (2479) [HTML] (0) [PDF 1.87 M] (17949)
    Abstract:
    Based on the current research status of multi agents system control theory and technology, the paper makes a detailed overview for unmanned ground systems. From two aspects of behaviour and task cooperative control for multi agents, the relevant theory and application problem is discussed. Moreover, some existed open problems are presented and a possible future development is proposed. For unmanned ground systems, cooperative control will be of great importance in promoting social and military benefits and maximizing the executive function of ground mission.
    2015,13(5):361-366, DOI: 10.6052/1672-6553-2014-064
    [Abstract] (1286) [HTML] (0) [PDF 826.19 K] (17841)
    Abstract:
    Dynamic and control systems often contain uncertain parameters that may result in uncertain predictions. In the interest of quantifying the effects of parameter uncertainties on response variability, this paper develops a stochastic response surface based method for the sensitivity analysis of uncertain parameters. Stochastic response surfaces were firstly constructed to describe the explicit relationships between uncertain parameters and responses. Then partial derivations were performed on the mathematical expressions of stochastic response surfaces in order to obtain sensitivity indices that simultaneously embody the effects of parameter means and standard deviations. Lastly, the developed method has been verified against a numerical cantilever beam containing uncertain geometric and material parameters. The sensitivity analysis results were compared with those given by the analysis of variance method.
    2014,12(3):225-229, DOI: 10.6052/1672-6553-2014-051
    [Abstract] (2456) [HTML] (0) [PDF 1.38 M] (17733)
    Abstract:
    Based on the staggered solution procedure of ANSYS and CFX software, the fluid structure coupling response of projectile during tail slapping has been researched. Structural response was simulated by using FEM and flow field was simulated by using inhomogeneous model and SST turbulence model. Finally, the influences of fluid structure coupling effect have been analyzed and the change law of body stress has been given.
    2013,11(1):12-19, DOI: 10.6052/1672-6553-2013-003
    [Abstract] (2431) [HTML] (0) [PDF 530.95 K] (17581)
    Abstract:
    The dynamics of the whole aero-engine system has always been the important part that cannot be neglected in the research and design of the engine, as the framework of the engine, the vibration of the casing directly reflects the level of the whole aero engine vibration. In this paper, an analysis was made on the research of the problems and fault classification of aero-engine casing dynamics, and an overview was made on the research of present situation, development trend, problems and solutions of the domestic and foreign of casing dynamics, which expanded the present situation of the Inclusiveness problems of aero-engine casing dynamics. Finally, some proposals were put forward for the development of the casing dynamics suitable for our country aero-engine technology level.
    2008,6(4):301-306, DOI:
    [Abstract] (1266) [HTML] (0) [PDF 0.00 Byte] (17310)
    Abstract:
    The problem of P and PI feedback control to a time delay system was investigated,with the emphasis on the determination of the feedback gains that ensured the asymptotical stability of the delayed system. By means of Lambert W function,the feedback gain of P control can be expressed explicitly,so that the optimal feedback gain can be easily obtained. For the system under a PI control,the stable region of the feedback gains was determined on the basis of stability switches and D subdivision,and the optimal feedback gains that enabled the system to admit maximal stable margin were figured out numerically by using Lambert W function. From the viewpoint of computation,the present method is much simpler than the available methods.
    2012,10(1):21-26, DOI:
    [Abstract] (867) [HTML] (0) [PDF 567.09 K] (17284)
    Abstract:
    A discrete finite dimensional dynamical model was built to describe the space large overall motion of tethered satellite system with an infinite dimensional viscoelastic tether in a long time. The tethered satellite system is a complex nolinear dynamic system. Considering the tether’s viscoelasticity, distributed mass and space form, the established improved bead model can meticulously describe the tether’s vertical and horizontal vibration. According to tether’s characteristic of tensile and not compressive, the slack tether unit model was set up to accurately reflect real stress of tether. The determination of the number of degrees of freedom of the system was studied. Based on numerical integral calculation, the dynamic response was obtained via numerical simulation of the deployment, retrievement and retainment process of tethered satellite system in a long time. The result is convergent. The simulation proves the important role of the stable equilibrium position in the dynamics of tethered space system.
    2014,12(2):183-187, DOI: 10.6052/1672-6553-2014-025
    [Abstract] (1397) [HTML] (0) [PDF 811.52 K] (17016)
    Abstract:
    PMSM due to little harmonic, high precision torque, commonly is used in the servo system and the high performance speed control system. In this paper,the physical model of PMSM is simplified and the mathematical model of the motor is established in order to facilitate research.Thispaper uses id=0 control manner which is the simplest manner is vector control methods,motor electromagnetic torque equation is established based on rotor field oriented vector control.The system model, speed and current control block are build and simulated with MATLAB/Simulink.Simulation results shows that the waveform is consistent with thoretical analysis,the model has fast response and small overshoot.The system runs stably with good dynamic and static characteristics. The simulation makes full use of modularization design. All the parameters and their influence on the system can be changed and observed.It also can easily validate the control strategies and select the most suitable one. So this kind of simulation is good for system design and adjusting and validating.
    2014,12(3):205-209, DOI: 10.6052/1672-6553-2014-059
    [Abstract] (2091) [HTML] (0) [PDF 467.15 K] (14514)
    Abstract:
    This paper investigated the passive nonlinear vibration control method used for energy absorbing in structures of spacecrafts. The structure and the dynamic model of the nonlinear energy sink which could adapt to the space environment were proposed. As nonlinear spring could not be acquired easily in reality, we proposed a new design for the NES based on employing an asymmetric NES force which was generated by two pairs of aligned permanent magnets. Then, the dynamic model for a cantilever beam structure coupled with nonlinear energy sink had been built theoretically. In addition, the passive vibration suppression effect of the nonlinear energy sink on the cantilever beam structure under transient excitation had been analyzed through Galerkin method and numerical analysis method. The results showed that the NES acquired up to 92% dissipation of the system energy imposed by shock excitation, hence the NES could adapt to the space environment and improve the reliability of space system.
    2014,12(3):283-288, DOI: 10.6052/1672-6553-2014-061
    [Abstract] (3050) [HTML] (0) [PDF 479.50 K] (13774)
    Abstract:
    A method was presented to analyze the nonlinear flutter. Based on this method, the flutter characteristics of the high aspect wing were illustrated. The numerical results show that the flutter speed is decreased when the first horizontal bending mode involved. Secondly, this study discussed how the main direction of the composite influenced the character of the nonlinear vibration and flutter, and established the method of the flutter clipping to the high aspect wing. And the result shows that the stiffness of structure can be changed by changing the main direction of the composite. It mainly changes the horizontal bending mode, makes the main direction tend to the trailing edge, and then makes the section line move to the leading edge. Further analyzing the nonlinear flutter reveals that it is the changing of the horizontal bending mode that causes the flutter speed change obviously. And by the section line of this mode moves ahead, the flutter speed will become larger. In the study, two examples were illustrated to validate its truthiness.
    2013,11(4):357-362, DOI: 10.6052/1672-6553-2013-041
    [Abstract] (1450) [HTML] (0) [PDF 350.50 K] (11955)
    Abstract:
    At present, the main task of designing a mounting system of automotive engine powertrain is to select appropriate stiffness, position and angle of mounting components so that free-vibration modal frequency of the mounting system can avert from the exciting-force frequency at the idle speed of the engine and the natural frequency of vibration of the vehicle body and that the decoupling degree of each mode shape is increased as far as possible, so as to improve the vibration-isolation effect of the mounting system. The design of a mounting system based on strict decoupling at predetermined frequencies is to make the modal frequencies of the designed mounting system completely equal to the frequencies predetermined in accordance with the frequency planning of automotive design, and to enable strict decoupling of each mode shape of each mode, i.e., the decoupling degree of vibration energy in every direction equals to 1. Based on a free-vibration equation for a mounting system, this paper presents an equation system for designing a mounting system with strict decoupling at predetermined frequencies, provides a solving method for this equation system by using the theory of generalized inverse matrix or method of constructing function, so as to provide an optimal design method more efficient and simpler than the current modal optimization method of mounting system. Relevant example has validated the correctness of equations and solving method of the strict-decoupling design at predetermined frequencies.
    2016,14(3):247-252, DOI: 10.6052/1672-6553-2015-052
    [Abstract] (1845) [HTML] (0) [PDF 2.18 M] (9075)
    Abstract:
    Tires are the only carrier of the contact between the vehicle and road surface. Their mechanical property is important for analysis and control on the vehicle dynamic response. At present, the tire simulation mostly focuses on the steady state model. But it can not describe the dynamic characteristic of the tire accurately. Therefore, it plays a significant role to add the dynamic tire model in the vehicle dynamics simulation. The tire friction model in the multi body dynamical software ADAMS is static, where the friction is regarded as a static value. However, in actual, the friction between the tire and road surface is dynamic, and it should be a dynamic function of the relative velocity and displacement. To this end, in this paper, the dynamic tire LuGre model using the Matlab/Simulink software is constructed. Through connecting the interface with Adams/Car, co simulation between the vehicle model and the simulink tire model is carried out in order to achieve the dynamic contact between tire and road and improve the accuracy of vehicle system analysis.
    2014,12(1):36-43, DOI: 10.6052/1672-6553-2013-110
    [Abstract] (2183) [HTML] (0) [PDF 2.22 M] (7639)
    Abstract:
    The coupling nonlinear dynamic model of dual rotor system was established by using finite element method, and then the critical speed of revolution and mode shape were calculated by using the software MATLAB. In addition, the unbalance responses of dual rotor system were studied, and the vibration performances in different speeds of dual rotor casing systems were obtained. The research provides a theoretical basis for the design of the dual rotors system in engineering.
    2014,12(3):253-258, DOI: 10.6052/1672-6553-2014-056
    [Abstract] (2074) [HTML] (0) [PDF 1.00 M] (6007)
    Abstract:
    Taking account of the structural stiffness and the low order vibration frequencies, two schemes of multi-objective topology optimization were proposed to obtain the best aircraft lifting-surface structural design. Based on penalized density theory, the scheme one (named as constrain method) is to convert the multi-objective optimization to single-objective optimization by considering the minimum structural mass as the objective with constraints of reference points displacements and the low order vibration frequencies. The scheme two (named as the combination of constrain method and criterion function method) settles the multi-objective optimization by defining combined compliance index (CCI) as the objective, with the constraints of volume fraction and the low order vibration frequencies. The CCI is the function of structural compliance and low order vibration frequencies. Numerical results demonstrate the proposed schemes not only realize reducing the structural mass but also raise the first and second order frequencies.
    2014,12(3):201-204, DOI: 10.6052/1672-6553-2014-048
    [Abstract] (2165) [HTML] (0) [PDF 296.79 K] (5664)
    Abstract:
    Non-linear factors cannot be avoided in the design of aircraft structures. In this paper, a two-degree-of-freedom airfoil and cubic stiffness nonlinearities in pitching degree-of-freedom operating in supersonic flight speed regimes has been analyzed. The averaging method and the theory of flutter were used to analyze the nonlinear dynamic system of the dualistic airfoil in the supersonic flow. Then the correctness of the theoretical calculation was verified by numerical calculation, and the analysis result was given.
    2014,12(1):62-66, DOI: 10.6052/1672-6553-2013-097
    [Abstract] (1570) [HTML] (0) [PDF 832.87 K] (5238)
    Abstract:
    A spline finite point method was presented to study the natural frequency of arch. The displacement mode shape function of the arch free vibration was simulated with a linear combination of cubic B spline. The free vibration frequency equation of arch structures was derived according to Hamilton principle, in which the effect of the dead load was considered. Meanwhile, the effect of the dead load on the natural frequency of arch structures was analyzed. The results show that the natural frequency of arch is reduced. The effect of influence depends on the stiffness of the arch itself. When the arch stiffness is certain, the bigger the rise span ration and the radius to thickness ration, the higher the effect of the dead load on the natural frequency of arch structures.

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