Time-Domain Analysis of Body Freedom Flutter Based on 6DOF Equation

The reduced weight and improved efficiency of modern aeronautical structures result in a decreasing separation of frequency ranges of rigid and elastic modes.Particularly,a high-aspect-ratio flexible flying wing is prone to body freedomflutter(BFF),which is a result of coupling of the rigid body short-periodmodewith 1st wing bendingmode.Accurate prediction of the BFF characteristics is helpful to reflect the attitude changes of the vehicle intuitively and design the active flutter suppression control law.Instead of using the rigid body mode,this work simulates the rigid bodymotion of the model by using the six-degree-of-freedom(6DOF)equation.A dynamicmesh generation strategy particularly suitable for BFF simulation of free flying aircraft is developed.An accurate Computational Fluid Dynamics/Computational Structural Dynamics/six-degree-of-freedom equation(CFD/CSD/6DOF)-based BFF prediction method is proposed.Firstly,the time-domain CFD/CSD method is used to calculate the static equilibrium state of the model.Based on this state,the CFD/CSD/6DOF equation is solved in time domain to evaluate the structural response of themodel.Then combinedwith the variable stiffnessmethod,the critical flutter point of the model is obtained.This method is applied to the BFF calculation of a flyingwing model.The calculation results of the BFF characteristics of the model agree well with those fromthe modalmethod andNastran software.Finally,the method is used to analyze the influence factors of BFF.The analysis results show that the flutter speed can be improved by either releasing plunge constraint or moving the center ofmass forward or increasing the pitch inertia.

Analysis on flutter performance of flexible photovoltaic support based on full-order method

Taking a three-cable flexible photovoltaic(PV)support structure as the research subject,a finite element model was established.Utilizing a full-order flutter analysis method,the flutter critical wind speed and flutter frequency of the flexible PV support structure at a tilt angle of 0°were calculated.The results showed good agreement with wind tunnel test data.Further analysis examined the pretension effects in the load-bearing and stabilizing cables on the natural frequency and flutter critical wind speed of the flexible PV support structure.The research findings indicate increasing the pretension in the load-bearing cables significantly raises the natural frequencies of the first four modes.Specifically,as the pretension in the load-bearing cables increases from 22 to 102 kN,the flutter critical wind speed rises from 17.1 to 21.6 m/s.By contrast,the pretension in the stabilizing cable has a smaller effect on the natural frequency and flutter critical wind speed of the flexible PV support structure.When the pretension in the stabilizing cable increased from 22 to 102 kN,the flutter critical wind speed increased from 17.1 to 17.7 m/s.For wind-resistant design of flexible PV support structures,it is recommended to prioritize increasing the pretension in the load-bearing cables to enhance the structural flutter performance.

基于Flutter的智能场景记账APP的设计与实现

综合了市面上记账类APP的功能并根据当下用户的一些需求设计了一款满足个人财务管理需求的同时基于智能记账且便捷、简单好用的记账APP,并通过Flutter搭建前端,Spring Boot搭建后端和MySQL数据库实现了这款智能场景记账APP,同时也将其部署在了服务器上。

基于Flutter的中老年智慧生活APP软件设计与实现

当前,中国的人口老龄化仍呈上升趋势,中老年人越来越频繁地使用手机和家电,容易出现困惑和忘记操作步骤的情况。基于此,文章基于FlutterUI框架、使用SpringBoot作为后台开发框架来开发了一款跨平台APP软件“步步有伴”,其中整个APP采用MVVM架构,后端程序采用MVC架构。开发的目标是帮助中老年人更好地了解和使用这些设备,提高生活质量。开发结果表明,软件可以帮助中老年人更好地管理自己的日常事务,并且帮助子女可以随时随地了解父母的待办事项和提醒事项,并及时提供帮助和支持。

基于Flutter 框架的高校师生协同平台的设计与实现

为保证高校师生信息传输安全,提高教学质量与工作效率,文章结合移动应用程序现有跨平台开发框架,并以济南大学已建成的数据中心作为数据支撑,设计出一套基于Flutter框架的高校师生协同平台。平台可实现用户信息、沟通记录、文档传输等内容本地化存储,同时集成教务、邮箱等办公应用,为高校师生提供集沟通、信息查询和应用办公于一体的移动服务,该平台的引入加速了济南大学数字化转型,进一步提升师生办公效率。

基于Vue和Flutter的经验库设计与实现

随着全球汽车工业的持续繁荣与快速发展,车辆设计和生产过程中的碰撞安全性能已成为评估车辆整体安全性的重要指标之一,其研究和优化显得尤为重要。然而,在车辆碰撞试验过程中积累的大量经验知识如何有效进行管理和共享,成为提升车辆安全性能的关键挑战。为应对这一挑战,文章深入研究了车辆碰撞试验过程中的经验知识管理需求,设计并实现了一个基于Vue和Flutter技术的经验库平台,为车辆碰撞试验过程中的经验知识提供全面、高效的管理和共享机制。该平台通过Vue开发网页端经验管理页面,提供丰富的数据展示和交互功能;同时,利用Flutter框架开发移动端应用,支持问题发布与解决方案的快速更新^([1])。

Mechanistic Insights into Roof-Dependent Macroreentrant Atrial Flutter with Endocardial Block of the Roof Line:A Case Report

Background:Epicardial roof-dependent atrial tachycardia is rare among macroreentrant tachycardias.The importance of epicardial structure or fiber involving septopulmonary bundle(SPB)has not been realized generally.Case presentation:A 74-year-old woman who underwent catheter ablation of atrial fibrillation previously accepted a second-time radiofrequency ablation due to atrial flutter.The mapping and entrainment results of the tachycardia tended to be an epicardial SPB-dependent macroreentrant atrial tachycardia and it was ablated to sinus rate at the first single targeting site,just located in the breakout site of SPB into the posterior wall(PW)of left atrial(LA).The twice-activation mapping of PW of LA also proved the presence of SPB.No recurrent arrhythmia was seen at follow-up at 3 months.Conclusion:In this case,an uncommon phenomenon was observed post-ablation for persistent atrial fibrillation,where the epicardial muscular structure of the LA-SPB was involved in atypical atrial flutter.This should be considered as a potential factor in such cases.Further similar cases may be required to improve diagnostic accuracy and to formulate effective ablation strategies for this type of tachycardia.

基于Flutter的今日早饭App功能设计与开发

当今中国社会正在飞速地向前发展,在这个信息化时代,由于人们对科技的热爱以及科技的发展,智能手机的发展趋势势不可挡,由此也促使了很多美食App的出现。该设计是基于AndroidFlutter移动平台美食菜谱系统来进行分析和设计的,设计一款早饭App,用户通过手机软件可以获得美食具体的菜谱信息、进行线上分享、获取流行菜谱等。文章简要介绍了App的功能以及实现方法,先对整个项目进行总体设计,对一些框架和界面进行整体的基本搭建,然后具体介绍每个模块,每个界面都有一定的功能,使读者了解基于Flutter的美食App设计与开发的一个流程,界面的清晰展示以及流畅的跳转,给用户操作带来一个更好的视觉体验,再配合一些好的组件或者框架,使项目更加完善,更好服务于客户。

基于Flutter的山羊孕测App设计与实现

目前大部分软件产品服务形式已逐步从传统单一的B端向多平台转变,但针对各平台单独开发将会是一个较大工作量、运维成本高、人力成本高的方案,涉及智慧畜牧的情况也是这样。文章介绍选用Flutter开发框架和Golang语言设计和实现一个跨平台的山羊孕测App,包括视频监控、即时通讯、异常通知等功能。利用Golang开发操作后端数据与Socket通信SDK包,使用Flutter开发框架调用SDK包编写一套程序代码进行跨端编译在Android、iOS两个平台运行。有效地提高了开发效率、性能的稳定,降低维护成本,加快对山羊孕测即时响应度。

基于Flutter的“文旅大同”APP设计与开发

大同市作为山西省第二大城市,是中国首批24个国家历史文化名城之一、中国古都之一、中国优秀旅游城市。为了更好地宣传大同,不断提升大同文化旅游产品的社会影响力,进而创造源源不断的经济收益,基于Flutter框架设计实现手机端软件——“文旅大同”移动APP。该APP的功能主要包括:大同小记、大同圈子(攻略、游记、分享、求助)和大同日志(美食、景区、文化、资讯)。该APP使得广大游客更方便快捷地查询大同各类文化旅游信息,对于宣传大同文化旅游,推动大同走向全国、走向世界具有重要意义。

基于Flutter的老年人服务平台

针对居家老人对附近医院及医疗服务系统不了解,对所处医院的强势科室不了解等问题,文中融合Android和Flutter技术开发了一款多功能老年人服务平台,该平台可以帮助居家老人对医院进行全面了解,并及时获悉所在医院相关信息。该老年人服务平台可以减少人力、物力的投入,提高医护工作效率,大大方便了老年人和医护工作者,拥有广阔的发展前景。

Revealing the Fluttering Motions of Mid-Water Trawl Codend Through Sea Trials:Case Study of Antarctic Krill Trawl Codend

The dynamic coupling between the fluttering motions and hydrodynamic characteristics of codend is essential in understanding the trawl selectivity through fish response and the drag force acting on the whole trawl.This study investigated the effect of towing speed,warp length,warp tension,and catch size on the fluttering motions of Antarctic krill trawl codend during net shooting,towing,and hauling by using sea trial data.The time-periodicity of codend oscillation was analyzed by the Morlet wavelet transform method.Results indicated that the period of codend oscillation was between 50 s and 90 s and showed an increasing trend with the warp tension but a decreased value at the towing stage.The coefficient amplitude of codend oscillation was between 0 and 4 at the net shooting and hauling stages,and between 0.2 and 0.6 at the towing stage.The amplitude of codend oscillation increased with the warp tension,towing speed,and catch size,but decreased with the increase of the warp length.In addition,the period of codend oscillation increased with the towing speed at the net shooting and hauling stages,but decreased at the towing stage.These results from codend fluttering motions can improve the understanding of fish behavior and gear shape that modify the hydrodynamic force on the codend instantaneously.

Geometrically Nonlinear Flutter Analysis Based on CFD/CSD Methods and Wind Tunnel Experimental Verification

This study presents a high-speed geometrically nonlinear flutter analysis calculation method based on the highprecision computational fluid dynamics/computational structural dynamics methods.In the proposed method,the aerodynamic simulation was conducted based on computational fluid dynamics,and the structural model was established using the nonlinear finite element model and tangential stiffness matrix.First,the equilibrium position was obtained using the nonlinear static aeroelastic iteration.Second,the structural modal under a steady aerodynamic load was extracted.Finally,the generalized displacement time curve was obtained by coupling the unsteady aerodynamics and linearized structure motion equations.Moreover,if the flutter is not at a critical state,the incoming flow dynamic pressure needs to be changed,and the above steps must be repeated until the vibration amplitude are equal.Furthermore,the high-speed geometrically nonlinear flutter of the wing-body assemblymodel with a high-aspect ratio was investigated,and the correctness of the method was verified using high-speed wind tunnel experiments.The results showed that the geometric nonlinearity of the large deformation of the wing caused in-plane bending to become a key factor in flutter characteristics and significantly decreased the dynamic pressure and frequency of the nonlinear flutter compared to those of the linear flutter.

Identification of the dominant loop of a dual-loop macro-reentry left atrial flutter without prior intervention using high-density mapping technology:A case report

BACKGROUND Left atrial flutter without prior cardiac interventions is uncommon,especially dual-loop macro-reentry atrial flutter.The critical step to ablate dual-loop macroreentry atrial flutter is to identify the dominant loop and key isthmus.Although entrainment mapping could help identify the dominant loop and key isthmus,it may alter or terminate tachycardia.High-density mapping allows the generation of electroanatomic maps without altering or terminating tachycardia.CASE SUMMARY Here,we report a case of symptomatic left atrial flutter without prior intervention.In this case,high-density mapping revealed a dual-loop macro-reentry around the mitral annulus and central scar of the anterior wall.The propagation result showed that the dominant loop was around the mitral annulus,and the key isthmus was between the central scar and mitral annulus.The atrial flutter terminated successfully after ablation was performed.CONCLUSION In this case,we demonstrate that high-density mapping technology may help identify the dominant loop of dual-loop atrial flutter without entrainment,which makes ablation easier.

Interval Finite Element Analysis of Wing Flutter

The influences of uncertainties in structural parameters on the flutter speed of wing are studied. On the basis of the deterministic flutter analysis model of wing, the uncertainties in structural parameters are considered and described by interval numbers. By virtue of first-order Taylor series expansion, the lower and upper bound curves of the transient decay rate coefficient versus wind velocity are given. So the interval estimation of the flutter critical wind speed of wing can be obtained, which is more reasonable than the point esti- mation obtained by the deterministic flutter analysis and provides the basis for the further non-probabilistic interval reliability analysis of wing flutter. The flow chart for interval fmite element model of flutter analysis of wing is given. The proposed interval finite element model and the stochastic finite element model for wing flutter analysis are compared by the examples of a three degrees of freedom airfoil and fuselage and a 15° sweptback wing, and the results have shown the effectiveness and feasibility of the presented model. The prominent advantage of the proposed interval finite element model is that only the bounds of uncertain parameters are required, and the probabilistic distribution densities or other statistical characteristics are not needed.

基于Flutter跨平台记账软件的设计与实现

记账在资金快速流动的现代社会成为人们生活中不可缺少的一部分。随着各式各样移动设备的普及,如何在各种设备之间实现财政数据的共享也成为一大问题。基于该设计并开发了一款基于Flutter跨平台智能记账软件,该软件在实现跨平台数据同步的同时,引入OCR(Opentical Character Rescognition,光学字符识别)技术实现批量记账,能够帮助用户进行高效的财务管理。

Flight Flutter Modal Parameters Identification with Atmospheric Turbulence Excitation Based on Wavelet Transformation

In view of the feature of flight flutter test data with atmospheric turbulence excitation, a method which combines wavelet transformation with random decrement technique for identifying flight flutter modal parameters is presented. This approach firstly uses random decrement technique to gain free decays corresponding to the acceleration response of the structure to some non-zero initial conditions. Then the continuous Morlet wavelet transformation of the free decays is performed; and the Parseval formula and residue theorem are used to simplify the transformation. The maximal wavelet transformation coefficients in different scales are searched out by means of band-filtering characteristic of Morlet wavelet, and then the modal parameters are identified according to the relationships with maximal modulus and angle of the wavelet transform. In addition, the condition of modal uncoupling is discussed according to variation trend of flight flutter modal parameters in the flight flutter state. The analysis results of simulation and flight flutter test data show that this approach is not only simple, effective and feasible, but also having good noise immunity.

Match Point Solution for Robust Flutter Analysis in Constant-Mach Prediction

This paper presents a method for robust flutter computation which uses flight altitude as the perturbation variable in order to obtain a match point solution. The air density and sound speed of standard atmosphere model are approximated as the polynomial function of altitude, such that the flight altitude becomes the single perturbation variable that describes the aeroelastic system. The uncertainties of generalized stiffness and damping are considered and the uncertain aeroelastic system can be formulated as linear fractional transformation （LFT） representation which is suitable for/.t analysis framework. Finally, the match point solutions of robust flutter margins can be computed with structured singular value （SSV） theory. The robust flutter analysis method provided in this paper is suitable for constant-Mach flight flutter test and provides valuable reference for flight envelope expansion.

基于Flutter开发框架的数据存储访问机制研究

移动端应用程序需要存储与访问的数据越来越多,而移动端设备的存储空间有限,很难满足用户需要,在进行移动端应用程序开发时,选择合适、高效的数据存储与访问机制受到普遍关注。针对Google推出的Flutter跨平台移动开发框架提供的key-value键值对、File文件、SQLite数据库和网络4种数据存储访问机制,深入阐述了它们的内在工作原理,给出了具体实现方法和实现代码。最后,根据4种数据存储访问机制各自的特点和实际的应用程序开发需求,分析了每种机制的应用场景。

FLUTTER SUPPRESSION USING DISTRIBUTED PIEZOELECTRIC ACTUATORS

The Flutter suppression using distributed piezoelectric actuators has been analyzed and tested. In constructing the finite element equation, effects of piezoelectric matrices are investigated. LQG method is used in designing the control law. In reducing the order of the control law, both balance realization and LK methods are used. For the rational approximation of the unsteady aerodynamic forces LS method is improved. In determining the piezoelectric constants d31 a new dynamic response method is developed. Laser vibrameter is used to pick up the model response and in ground resonance test the model is excited by piezoelectric actuators. Reasonable agreement of the wind tunnel flutter suppression test with calculated results is obtained.