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Behavior of Concrete Under Compressive Load01:23

Behavior of Concrete Under Compressive Load

143
Concrete exhibits specific behaviors under different compressive loads. Understanding this is crucial for understanding its structural integrity. When concrete undergoes uniaxial compression, it tends to develop cracks that run parallel to the direction of the force. These parallel cracks stem from localized tensile stresses that occur perpendicular to the compression direction. Additionally, angled cracks may appear due to the formation of shear planes.
As the concrete specimen fractures under...
143
Plastic Behavior01:21

Plastic Behavior

186
A material's elastic behavior is characterized by the disappearance of stress once the load is removed, allowing the material to return to its original state. However, when stress surpasses the yield point, yielding commences, marking the onset of plastic deformation or permanent set. This change from elastic to plastic behavior is influenced by the peak stress value and the duration before the load is removed. An intriguing observation occurs when a specimen is loaded, unloaded, and...
186
Members Made of Elastoplastic Material01:19

Members Made of Elastoplastic Material

93
The behavior of elastoplastic materials under bending stresses, particularly in structural members with rectangular cross-sections, is crucial for predicting material responses and understanding failure modes. Initially, when a bending moment is applied, the stress distribution across the section follows Hooke's Law and is linear and elastic. This distribution means the stress increases from the neutral axis to the maximum at the outer fibers, up to the elastic limit.
As the bending moment...
93
Dynamic Modulus of Elasticity of Concrete01:16

Dynamic Modulus of Elasticity of Concrete

254
The dynamic modulus of elasticity assesses how a concrete structure deforms under impact or dynamic loads. It is typically higher than the static modulus of elasticity, measured under slow, steady loading conditions.
The sonic test is a common method to determine the dynamic modulus. In this test, a concrete beam, sized either 6 x 6 x 30 inches or 4 x 4 x 20 inches, is clamped at its center. Vibrations are initiated at one end of the beam by an electromagnetic exciter unit powered by...
254
Normal Strain under Axial Loading01:20

Normal Strain under Axial Loading

440
Normal strain under axial loading is an important concept in the field of mechanics of materials. Axial loading implies the application of a force along the axis of a material, like a column or bar. This force can either compress or stretch the material. In the context of axial loading, normal strain is the deformation experienced by the material in the direction of the loading force. It's calculated as the change in length divided by the original length of the material. This unitless ratio...
440
Relation between Poisson's ratio, Modulus of Elasticity and Modulus of Rigidity01:15

Relation between Poisson's ratio, Modulus of Elasticity and Modulus of Rigidity

249
Deformation occurs in axial and transverse directions when an axial load is applied to a slender bar. This deformation impacts the cubic element within the bar, transforming it into either a rectangular parallelepiped or a rhombus, contingent on its orientation. This transformation process induces shearing strain. Axial loading elicits both shearing and normal strains. Applying an axial load instigates equal normal and shearing stresses on elements oriented at a 45° angle to the load axis.
249

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Related Experiment Video

Updated: Jun 3, 2025

Cutting Procedures, Tensile Testing, and Ageing of Flexible Unidirectional Composite Laminates
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Cutting Procedures, Tensile Testing, and Ageing of Flexible Unidirectional Composite Laminates

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Dynamic In-Plane Compression and Fracture Growth in a Quasi-Isotropic Carbon-Fiber-Reinforced Polymer Composite.

Yogesh Kumar1, Mohammad Rezasefat1, Zahra Zaiemyekeh1

  • 1Department of Mechanical Engineering, University of Alberta, Edmonton, AB T6G 2R3, Canada.

Materials (Basel, Switzerland)
|January 8, 2025
PubMed
Summary

This study investigates carbon-fiber composites under compression, revealing strain-rate effects on failure modes like kink bands and interlaminar cracks. A viscoelastic model characterizes dynamic behavior.

Keywords:
carbon-fiber-reinforced polymercrack speeddigital image correlationfracture planehighstrain ratein-plane compression

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A Method for Studying the Temperature Dependence of Dynamic Fracture and Fragmentation
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Area of Science:

  • Materials Science
  • Mechanical Engineering
  • Composite Materials

Background:

  • Carbon-fiber composites are crucial in aerospace and automotive industries.
  • Understanding their behavior under dynamic loading is vital for safety and performance.
  • Quasi-isotropic layups offer balanced properties but require detailed failure analysis.

Purpose of the Study:

  • To experimentally investigate the quasi-static and dynamic behavior of quasi-isotropic carbon-fiber composites under in-plane compression.
  • To quantify strain-rate dependency of mechanical properties and failure mechanisms.
  • To model the dynamic stress-strain response using a viscoelastic constitutive model.

Main Methods:

  • Experimental testing of composites at strain rates from 4×10⁻⁵ to 1200 s⁻¹.
  • Advanced camera systems for observing failure propagation and damage morphology.
  • Post-mortem analysis to identify failure modes (fiber bridging, kink bands, interlaminar failure).
  • Determination of crack speeds during failure.
  • Application of a modified Zhu-Wang-Tang viscoelastic model.

Main Results:

  • Quantified strain-rate-dependent in-plane compressive strength, failure strength, and stiffness.
  • Observed failure mechanisms including fiber bridging, kink band formation, and dominant interlaminar failure.
  • Measured crack propagation speeds in primary/secondary cracks and participating interfaces.
  • Successfully characterized dynamic stress-strain behavior with the viscoelastic model.

Conclusions:

  • Strain rate significantly influences the failure mechanisms and mechanical response of quasi-isotropic carbon-fiber composites.
  • Interlaminar failure and kink band formation are critical failure modes under compression.
  • The modified Zhu-Wang-Tang model provides a viable approach for predicting dynamic compressive behavior.