2. 您的位置
3. 首页
4. 会议论文
5. Numerical and experimental investigation of dynamic behavior of representative tail leading edges un

Numerical and experimental investigation of dynamic behavior of representative tail leading edges un

来源 :2nd International Conference on Lmpact Loading of Structural | 被引量 : 0次 | 上传用户：wangtianxin1818

【摘 要】

：

　　In order to improve the anti-bird strike performance of civil aircraft horizontal stabilizer leading edge Structures,a methodology combined finite element s

【作 者】

：

Xianghao Meng Yulong Li Zhongbin Tang Jun Liu 

【机 构】

：

NorthwesternPolytechnicalUniversity,Xi'an,China;FundamentalScienceonAircraftStructuralMechanicsandS

【出 处】

：

2nd International Conference on Lmpact Loading of Structural

【发表日期】

：

2018年5期

【关键词】

：

Bird strike Bird strike test Simulation SPH 

下载到本地 , 更方便阅读

下载此文 赞助VIP

声明 : 本文档内容版权归属内容提供方 , 如果您对本文有版权争议 , 可与客服联系进行内容授权或下架

论文部分内容阅读

　　In order to improve the anti-bird strike performance of civil aircraft horizontal stabilizer leading edge Structures,a methodology combined finite element simulation and bird strike test was used to study the anti-bird strike performance of three representative horizontal stabilizer leading edge structures.

其他文献

Experimental and Numerical Studies of Steel-PLA Composite Sandwich Panels under Blast Loading

　　Sandwich panels have been proven to be practical for protecting civil and vehicular objects under intensive impact load such as close-in detonation of high

会议

AuxeticDouble arrowSandwichImpactFinite element

A New Measurement Method of Relative Magnetic Permeability for Evaluation on Strain-induced Martensi

　　In the previous study,in order to evaluate the strain-induced martensitic transformation(SIMT)in the austenitic stainless steels continuously during deforma

会议

SUS304 Stainless SteelRelative Magnetic PermeabilityMartensitic Transformation

Theoretical Model of the Expansion of Metal Tubes

　　The expansion of the metal tube is always used as energy absorber.In this study,a new theoretical model of the expanding metal tube is developed.

会议

Energy AbsorberTube ExpansionSEA

Protection of Structural Elements against Explosive and Impact Loading

　　The aim of this work is numerical simulation of stress-strain state and destructions of barriers and protective layers under the influence of the products o

会议

ProtectionImpact LoadingPorous Materials

Effect of Ply Orientation on Energy-Absorbing Characteristics of Composite C-Channels Under Axial Co

　　Low speed axial crushing test was conducted on T700/MTM28 composite thin-walled specimens with different lay-up.The effect of ply orientation on energy-abso

会议

Thin-walled C-channelsLay-upFailure ModesEnergy-Absorbing Characteristics

Elasto-plastic dynamic response of ship plates to slamming load

　　Ship slamming is a phenomenon that the ship hull structure impacted by water when the ship sailing in waves.It happens when the relative velocity of the shi

会议

Ship slammingElasto-plastic responseMoving loadDynamic Load Factor (DLF)Nonl

The Effect Of Human Body Positioning On Neck Injuries During Compressive Impacts

　　Motor vehicle accident is the lead cause to the cervical spine injuries causing serious to fatal severity levels.The main reasons of these injuries are due

会议

Finite element neck modelcervical spineneck injuryhead-first impact

A Study on Change in Temperature of Pure Aluminum During Compressive Test at Higher Strain Rate Base

　　In quasi-static experiments,the thermal energy releases to outside faster than the speed of deformation and the temperature rise is insignificant.On the oth

会议

Impact CompressionSplit Hopkinson Pressure BarChange in TemperatureInfrared R

Influence of confinement on unit load devices subjected to internal blast loading

　　Unit Load Devices(ULDs)are used to store freight or luggage safely in the lower deck of wide boded aircraft.A potential risk to aircraft is an explosion tha

会议

Blast loadingUnit Load DevicesVentingAluminium PlatesExperiments

Application of Reverse Engineering for Large Airplanes Comprehensive Impact Modeling

　　Available large computer clusters and software capable to generate results using parallel computing allows consideration of detailed airplane model structur

会议

Reverse EngineeringImpact SimulationsLarge airplanes