Review of Solid Mechanics I
1. Concept of Stress and Strain
- Rigid body is an idealized model, but in reality, objects deform under forces.
- Stress ( ( \sigma ) ): Measures the force per unit area causing deformation.
- Strain ( ( \varepsilon ) ): Measures the relative deformation in response to stress.
- Elastic modulus (Young’s modulus, ( E ) ): Defines the relationship between stress and strain.
Stress in a Prismatic Bar (Under Tension)
For a prismatic bar with axial force ( P ) and cross-sectional area ( A ):
[ \sigma = \frac{P}{A} ]
Strain in a Prismatic Bar
For a bar of original length ( L ) that undergoes elongation ( \delta ):
[ \varepsilon = \frac{\delta}{L} ]
Assumptions:
- Uniform deformation.
- Loads act through the centroid.
- The material is homogeneous.
2. Stress-Strain Diagram
- Elastic region: The material returns to its original shape when stress is removed.
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Plastic region: Permanent deformation occurs after yielding.
- Proportional limit (A): The region where stress and strain are proportional.
In solid mechanics, the proportional limit is the region where stress and strain have a linear relationship. This follows Hooke’s Law, which states:
[ \sigma = E \varepsilon ]
where:
- ( \sigma ) = stress (force per unit area, measured in Pascals, Pa)
- ( \varepsilon ) = strain (dimensionless, ratio of deformation to original length)
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( E ) = Young’s modulus (elastic modulus, measures material stiffness, in Pascals)
- Young’s modulus (( E )) is a material property that defines how much a material deforms under stress.
- A higher ( E ) means the material is stiffer (harder to deform).
- A lower ( E ) means the material is more flexible.
For example:
- Steel has a high ( E ) → it resists deformation.
-
Rubber has a low ( E ) → it stretches easily.
- The proportional limit (Point A) is the point on the stress-strain curve where stress and strain are still proportional.
- Before reaching this point, the material fully obeys Hooke’s Law.
- Beyond this point, the stress-strain relationship becomes nonlinear, and permanent deformation may begin.
- Engineering stress: Uses the original cross-sectional area.
- True stress: Uses the updated cross-section.
3. Linear Elasticity and Hooke’s Law
Hooke’s Law (Axial Loading)
For an axially loaded member:
[ \sigma = E \varepsilon ]
Using force equilibrium and displacement relations:
[ \delta = \frac{PL}{EA} ]
where:
- ( E ) = Young’s modulus
- ( A ) = Cross-sectional area
- ( L ) = Length
- ( P ) = Applied load
[ P = \frac{EA}{L} \delta ]
which resembles Hooke’s law for a spring: ( F = kx ).
Derivation and Explanation of Axial Deformation Formula
When an axial force ( P ) is applied to a prismatic bar (a bar with uniform cross-section), the bar stretches or compresses. The amount of elongation or shortening is given by:
[ \delta = \frac{PL}{EA} ]
where:
- ( \delta ) = Axial deformation (elongation or compression)
- ( P ) = Axial force applied
- ( L ) = Original length of the bar
- ( E ) = Young’s modulus (material stiffness)
- ( A ) = Cross-sectional area of the bar
1. Force Equilibrium and Stress-Strain Relations
(1) Stress Definition
Stress ( \sigma ) in the bar is given by:
[ \sigma = \frac{P}{A} ]
Since Hooke’s Law states that stress and strain are proportional in the elastic region:
[ \sigma = E \varepsilon ]
where:
- ( \varepsilon ) = strain = relative deformation.
(2) Strain Definition
Strain is defined as:
[ \varepsilon = \frac{\delta}{L} ]
Substituting ( \sigma = \frac{P}{A} ) into Hooke’s Law:
[ \frac{P}{A} = E \varepsilon ]
Since ( \varepsilon = \frac{\delta}{L} ), we substitute:
[ \frac{P}{A} = E \frac{\delta}{L} ]
Rearranging for ( \delta ):
[ \delta = \frac{PL}{EA} ]
which is the axial deformation formula.
2. Rearranging the Formula
The equation can also be rewritten in terms of force:
[ P = \frac{EA}{L} \delta ]
This equation shows that:
- The restoring force ( P ) in an axially loaded bar acts like a spring, where the term ( \frac{EA}{L} ) represents the stiffness of the bar.
-
The form of the equation is similar to Hooke’s Law for a spring:
[ F = kx ]
where:
- ( k = \frac{EA}{L} ) (stiffness of the bar),
- ( x = \delta ) (displacement),
- ( F = P ) (applied force).
Thus, an elastic bar under axial load behaves like a linear elastic spring.
3. Interpretation
✅ What This Equation Tells Us
- Larger ( P ) → Larger ( \delta ): More force leads to more elongation.
- Larger ( L ) → Larger ( \delta ): Longer bars deform more for the same force.
- Larger ( E ) or ( A ) → Smaller ( \delta ): A stiffer material (high ( E )) or a thicker bar (large ( A )) deforms less.
❌ When This Formula Does NOT Work
- Material is beyond the elastic limit (plastic deformation occurs).
- Cross-section is not uniform (requires integration).
- Non-axial loading (torsion or bending is involved).
Poisson’s Ratio: Definition, Concept, and Applications
1. What is Poisson’s Ratio?
When a material is stretched in one direction, it contracts in the perpendicular directions. Similarly, when compressed, it expands laterally.
This behavior is quantified by Poisson’s ratio ( \nu ), which is defined as:
[ \nu = -\frac{\text{Lateral strain}}{\text{Axial strain}} ]
where:
- Lateral strain ( \varepsilon_{\text{lat}} = \frac{\Delta d}{d} ) (change in width/diameter per unit width)
- Axial strain ( \varepsilon_{\text{ax}} = \frac{\Delta L}{L} ) (change in length per unit length)
The negative sign ensures ( \nu ) is positive, since stretching (positive axial strain) causes contraction (negative lateral strain), and vice versa.
2. Interpretation of Poisson’s Ratio
- Higher Poisson’s ratio (( \nu \approx 0.5 )): Material is highly compressible laterally (e.g., rubber).
- Lower Poisson’s ratio (( \nu \approx 0 )): Material shows almost no lateral change (e.g., cork).
- Negative Poisson’s ratio (( \nu < 0 )): The material expands laterally when stretched, called an auxetic material.
Common Values of Poisson’s Ratio
| Material | Poisson’s Ratio (( \nu )) | |————-|——————| | Rubber | 0.49 - 0.50 | | Steel | 0.27 - 0.30 | | Aluminum | 0.33 | | Concrete | 0.15 - 0.20 | | Cork | 0.0 (no lateral contraction) | | Auxetic Materials | Negative ( \nu ) |
3. Relationship with Elastic Moduli
Poisson’s ratio connects different elastic properties of a material.
(1) Shear Modulus and Young’s Modulus
The shear modulus ( G ) (modulus of rigidity) is related to Young’s modulus ( E ) by:
[ G = \frac{E}{2(1+\nu)} ]
- If ( \nu ) is high, ( G ) is lower → material resists shear deformation less.
- If ( \nu ) is low, ( G ) is higher → material resists shear more.
(2) Bulk Modulus and Young’s Modulus
The bulk modulus ( K ) (resistance to uniform compression) is:
[ K = \frac{E}{3(1 - 2\nu)} ]
- If ( \nu \approx 0.5 ), bulk modulus is very high, meaning material is nearly incompressible (like rubber).
- If ( \nu \approx 0 ), bulk modulus is smaller, meaning material compresses more easily (like foam or cork).
4. Physical Meaning of Poisson’s Ratio
(1) Stretching a Rubber Band
- When you pull a rubber band, it becomes thinner.
- Rubber has a high Poisson’s ratio (~0.5), meaning it contracts significantly in width when stretched.
(2) Compressing a Sponge
- A sponge compresses easily in all directions.
- Its Poisson’s ratio is low, meaning lateral contraction is minimal.
(3) Cork vs. Rubber
- Cork has ( \nu \approx 0 ), meaning it does not contract laterally.
- That’s why wine corks are easy to insert into a bottle—they don’t expand sideways when pushed in.
5. Special Case: Auxetic Materials (( \nu < 0 ))
- Auxetic materials expand laterally when stretched (opposite of normal materials).
- They have applications in biomechanics, flexible armor, and shock absorption.
- Example: Some foams and engineered structures exhibit negative Poisson’s ratio.
Shear and Torsion in Solid Mechanics
1. Shear Stress and Shear Strain
Shear stress occurs when a force is applied parallel to a surface rather than perpendicular (as in normal stress). This type of stress deforms the material by causing adjacent layers to slide over each other.
(1) Shear Stress ( \tau )
Shear stress is defined as:
[ \tau = \frac{F}{A} ]
where:
- ( \tau ) = Shear stress (Pa)
- ( F ) = Applied force parallel to the surface (N)
- ( A ) = Area on which the force acts (m²)
(2) Shear Strain ( \gamma )
Shear strain is the deformation due to shear stress, defined as:
[ \gamma = \frac{\Delta x}{h} = \tan \theta \approx \theta ]
where:
- ( \gamma ) = Shear strain (dimensionless)
- ( \Delta x ) = Lateral displacement (m)
- ( h ) = Height of the material (m)
- ( \theta ) = Angle of deformation in radians
2. Hooke’s Law for Shear
Similar to Hooke’s Law for normal stress, the shear stress-strain relationship is:
[ \tau = G \gamma ]
where:
- ( G ) = Shear modulus (modulus of rigidity) (Pa)
- ( \gamma ) = Shear strain
Relationship Between Young’s Modulus ( E ) and Shear Modulus ( G )
The shear modulus ( G ) is related to Young’s modulus ( E ) and Poisson’s ratio ( \nu ) by:
[ G = \frac{E}{2(1 + \nu)} ]
- If ( G ) is high, the material resists shearing (e.g., steel).
- If ( G ) is low, the material deforms easily in shear (e.g., rubber).
3. Torsion in Circular Shafts
Torsion occurs when a circular shaft is twisted due to a torque ( T ). This generates shear stress inside the shaft.
(1) Shear Strain in Torsion
The shear strain ( \gamma ) at a distance ( r ) from the center of the shaft is:
[ \gamma = \frac{\phi r}{L} ]
where:
- ( \phi ) = Angle of twist (radians)
- ( r ) = Radial distance from the center (m)
- ( L ) = Length of the shaft (m)
(2) Shear Stress in Torsion
Using Hooke’s Law:
[ \tau = G \gamma ]
Substituting ( \gamma ):
[ \tau = G \frac{\phi r}{L} ]
(3) Torque and Polar Moment of Inertia
The total torque ( T ) in the shaft is given by:
[ T = G I_p \frac{\phi}{L} ]
where:
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( I_p ) = Polar moment of inertia, which depends on the cross-sectional area:
[ I_p = \int_A r^2 dA ]
For a solid circular shaft of radius ( R ):
[ I_p = \frac{\pi R^4}{2} ]
For a hollow circular shaft (outer radius ( R_o ), inner radius ( R_i )):
[ I_p = \frac{\pi}{2} (R_o^4 - R_i^4) ]
4. Key Insights
✅ Shear and Torsion in Materials
- Shear stress is caused by forces parallel to a surface.
- Torsion is caused by rotational forces in circular shafts.
- Both follow Hooke’s Law, with shear stress proportional to strain.
✅ Material Properties Affect Shear and Torsion
- High ( G ) (e.g., steel) → Resists shear and torsion.
- Low ( G ) (e.g., rubber) → Easily deforms under shear forces.
✅ Torsion Design Considerations
- Larger radius ( R ) → Higher resistance to torsion (( I_p \propto R^4 )).
- Hollow shafts are more efficient than solid shafts (high strength with less weight).
Understanding shear stress and torsion is essential for designing mechanical components like shafts, gears, and structural beams! 🚀
4. Strain Energy
Stored Energy in an Elastic Bar
For a bar subjected to axial force ( P ):
[ U = \int_0^{\delta} P \, d\delta = \frac{1}{2} P \delta ]
Using ( \delta = \frac{PL}{EA} ):
[ U = \frac{P^2 L}{2EA} ]
Strain Energy Density
[ u = \frac{U}{V} = \frac{1}{2} \sigma \varepsilon ]
For a bar with volume ( V = AL ):
[ U = \frac{1}{2} \frac{P^2 L}{EA} = \frac{1}{2} \frac{\sigma^2}{E} A L ]
5. Stress Concentration
- Stress concentration occurs due to geometric discontinuities (holes, sharp corners, etc.).
- Saint-Venant’s principle: Stresses become uniform at a distance from the load application point.
- Maximum stress ( \sigma_{\text{max}} ) is higher than average stress.
[ \sigma_{\text{max}} = K_t \sigma_{\text{avg}} ]
where ( K_t ) is the stress concentration factor.
6. Allowable Stress and Factor of Safety
To prevent failure, we define the factor of safety (SF):
[ SF = \frac{\text{actual strength}}{\text{required strength}} ]
For yielding:
[ SF = \frac{\sigma_y}{\sigma_{\text{actual}}} ]
where ( \sigma_y ) is the yield stress.
Design Considerations:
- ( SF > 1 ) ensures safety.
- Higher ( SF ) is used for critical structures (e.g., bridges, aircraft).
7. Summary
✅ Key Concepts
- Stress and Strain: Fundamental properties of material deformation.
- Hooke’s Law: Describes linear elasticity.
- Poisson’s Ratio: Relationship between axial and lateral strain.
- Strain Energy: Energy stored in elastic deformation.
- Stress Concentration: Localized stress increase due to discontinuities.
- Allowable Stress & Safety Factor: Ensures safe structural design.