Rate effect - Globe Thesis

Keyword [Rate effect] Result: 21 - 40 \| Page: 2 of 7
21.	Research On Dynamic And Penetration Properties Of The Three-dimendional Orthogonal Woven Glass Fiber Composites
22.	Study On The Static-dynamic Mechanical Propertie Of Heterogeneous Composite Materials
23.	Theoretical Analysis And Numerical Simulation Of The Dynamic Response Of Metal Foam Under Impact Loading
24.	Impact Tensile Properties And Finite Element Analysis Of3-D Angle-interlock Carbon Woven Fabric
25.	High Strain Rate Compression Property And Finite Element Analysis Of3D Woven Composites
26.	Investigation On Interfacial Behaviors Of CNTs And Metal Interconnect Materials
27.	Study On Dynamic Response Of Hollow Sphere/aluminum Composite Foam Sandwich-like Plate Structures
28.	Yield Behavior Of Aluminum Alloy Foams And NOMEX Honeycombs
29.	Experimental And Numerical Analyses Of The Strain Rate Effect Of Tensile Behavior Of3D Woven Fabrics&Mechanical Testing And Numerical Analyses Of Novel Honeycomb Sandwich Structures
30.	Evaluation Method And Application Of Coal Burst Performance Under The Effect Of Loading Rate
31.	High Frequency Vibration Effects Inrotary Ultrasonic Machining Hard-brittle Material
32.	Study On In-plane Compressive Strength Of Carbon Fiber Reinforced Laminated Composites
33.	Study On The Effect Of In-plane Size And Strain Rate Of Honeycomb Aluminum Alloy
34.	Mechanical Property Study Of CFRP Laminates Subjected To High Impact Compressive Loads
35.	Research On The Impact Behavior And Dynamic Strength Of 3-D Woven Composite
36.	Local Stress Calculation Method In Cell-based Finite Element Model Of Cellular Materials And Its Application
37.	Yield Behavior And High Temperature Deformation Of Medical Ti-Cu Alloy
38.	Mechanical Properties And Deformation Mechanisms Of Zr-Based Metallic Glasses And Their Composites
39.	The Three-dimensional Hybrid Method And Experimental Research Of Glass Fiber Reinforced Polypropylene Material
40.	Peridynamic Simulation For The Rate Effect Of Impact Damage In Composite Laminate
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