不对称的曲边界层:λ-测试
Nathan Vani1, Alejandro Ibarra1, José Bico1
1Physique et Mécanique des Milieux Hétérogènes, CNRS UMR7636, Ecole Supérieure de Physique et Chimie Industrielles de Paris, Paris Sciences et Lettres Research University, Sorbonne Université, Université de Paris, Paris 75005, France.
概括
我们发现,拉拉的带的结合角度揭示了它们的曲刚度,挑战了关于薄的假设. 这一发现使膜特征的新视觉测试成为可能.
科学领域:
- 材料科学与工程 材料科学与工程
- 机械工程 机械工程
- 软物质物理学 软物质物理学
背景情况:
- 薄外通常被认为在较大的拉力负荷下具有可以忽略不计的曲刚度.
- 了解绑定结构的机制对于设计灵活的材料和设备至关重要.
- 非对称结构在预测它们的机械反应方面存在独特的挑战.
研究的目的:
- 为了研究两个不对称地绑定的带拉开的机制.
- 描述弹性结点及其与拉力和曲刚性的关系.
- 挑战传统的假设,忽视在压力下的薄外的曲刚性.
主要方法:
- 关于绑定不对称的带带的机制的实验研究.
- 弹性结点作为曲边界层的特征.
- 分析旋转反应及其对不对称性和拉力的依赖.
主要成果:
- 结合角度作为曲刚度的宏观签名,随着拉力而减少.
- 旋转反应表现出非线性和普遍的行为,独立于不对称比率.
- 该研究挑战了在显著的拉伸负荷下,在薄外中忽视曲刚度的忽视.
结论:
- 结合角是曲刚性的可靠指标,即使在较大的拉力下.
- 介绍了一种新的视觉测量技术,即兰巴测试,用于膜特征.
- 结果需要重新评估工程应用中薄外的机械假设.
更多相关视频
相关概念视频
Boundary Layer Characteristics
28
When a fluid encounters a solid surface, a boundary layer forms due to the interaction between the fluid's motion and the stationary surface. This phenomenon is characterized by a thin region adjacent to the surface where viscous forces dominate, influencing the fluid's velocity profile. The development of the boundary layer begins at the leading edge of the surface and evolves as the fluid moves downstream.As the fluid flows over the surface, friction between the fluid and the wall slows down...
28
Unsymmetric Bending
296
Unsymmetrical bending occurs when the bending moment applied to a structural member does not align with its principal axis. This misalignment leads to complex stress distributions and deflection patterns that differ from those in symmetrical bending, and are essential for designing structures to withstand different loading conditions. In unsymmetrical bending, the neutral axis—where stress is zero—does not necessarily align with the geometric axes of the cross-section. The...
296
Unsymmetric Bending - Angle of Neutral Axis
260
Unsymmetrical bending occurs when a structural member is subjected to bending moments in a plane that does not align with the member's principal axes. This scenario typically arises in beams and other structural components when loads are applied at non-ideal angles, introducing complexities in stress analysis.
When a bending moment is applied at an angle θ concerning the vertical axis of a symmetrical member, it can be resolved into components along the member's principal...
When a bending moment is applied at an angle θ concerning the vertical axis of a symmetrical member, it can be resolved into components along the member's principal...
260
Symmetric Member in Bending
164
In the study of the mechanics of materials, analyzing the behavior of prismatic members under opposing couples is crucial for understanding internal stress distributions, which are essential for structural design. When subjected to couples, a prismatic member experiences internal forces that maintain equilibrium. A couple, characterized by two equal and opposite forces, creates a moment but no resultant force. The internal forces at any section cut of the member must balance these external...
164
Deformations in a Symmetric Member in Bending
159
When analyzing the deformation of a symmetric prismatic member subjected to bending by equal and opposite couples, it becomes clear that as the member bends, the originally straight lines on its wider faces curve into circular arcs, with a constant radius centered at a point known as Point C. This phenomenon helps to understand the stress and strain distribution within the member more clearly.
When the member is segmented into tiny cubic elements, it is observed that the primary stress...
When the member is segmented into tiny cubic elements, it is observed that the primary stress...
159
Lift
34
Lift is a fundamental aerodynamic force that acts perpendicular to the direction of airflow. It plays a central role in achieving and sustaining flight and in stabilizing various vehicles. Lift primarily originates from pressure differences created across surfaces, such as an airfoil. A lower pressure region forms above the wing, while a higher pressure region forms below it, generating an upward force. This differential results from the shape and orientation of the airfoil, enabling the wing...
34


