Internal Biomechanics: Tissue and Muscle Mechanics Flashcards

Internal Biomechanics: Tissue and Muscle Mechanics

Overview of Internal Biomechanics

  • Core Topics:     * Tissue mechanics.     * Muscle mechanics (including eccentric and concentric actions).     * Interaction with the environment.     * Effect of internal and external forces.

Forces, Deformation, and Injury Loading

  • Experimental Context: Rubber Band Groups (G1 and G2):     * Group 1 (G1): Consists of 1 rubber band.     * Group 2 (G2): Consists of 5 rubber bands.
  • Loading Scenario A: Applying Equal Force:     * When the same amount of force is applied to both groups separately, it results in unequal deformation (Δ length\Delta\text{ length}).     * Result: G1 (1 rubber band) is easy to break and exhibits greater deformation. G2 (5 rubber bands) is harder to break and exhibits smaller deformation.
  • Loading Scenario B: Applying Equal Deformation:     * When G1 and G2 are lengthened to the same distance separately, it results from unequal forces.     * Result: It requires significantly more force to lengthen G2 to the same distance as G1.
  • Key Principle: Force and deformation outcomes depend on the angle of application and the amount of force applied.

Stress: Standardizing the Loading

  • Definition of Stress (σ\sigma):     * Stress is a normalized loading to the analysis plane.     * Verbatim Definition: "The intensity of the distributed force, F, distributed over an area, A."     * Formula:         σ=FA\sigma = \frac{F}{A}     * Units: N/m2N/m^2 (Newtons per square meter) or Pascals (PaPa).     * Variables:         * FF: Internal force.         * AA: Internal area (analysis plane).
  • Conceptual Explanation: Stress represents how much force is applied to a specific amount of area.

Anatomical Directions, Planes, and Motion

  • Anatomical Position Definitions:     * Anterior: Forward (e.g., Patella is anterior to the knee joint).     * Posterior: Backward.     * Superior: Upward (e.g., Humerus is superior to the elbow joint).     * Inferior: Downward (e.g., Tibia is inferior to the knee joint).     * Medial: Toward the middle/midline (e.g., Ulnar is medial to the radius).     * Lateral: Toward the sides (e.g., Radius is lateral to the ulnar).
  • Cardinal Planes of the Body:     1. Sagittal Plane: A vertical plane dividing the body into right and left parts.     2. Frontal (Coronal) Plane: Divides the body into anterior and posterior parts.     3. Transverse (Horizontal) Plane: Divides the body into superior and inferior parts.
  • Joint Motion Principles:     * All segments rotate about a joint center.     * Joint motions are defined based on anatomical positions, planes, and axes.     * Examples: The lower leg rotates about the knee joint; the foot rotates about the ankle joint.

Types of Loading (Hsieh, Chapter 8)

  • 1. Tensile Loading (Pull/Stretch):     * Mechanism: Loading applied along the longitudinal axis of the body and perpendicular to the analysis plane.     * Action: Forces pull apart, causing the body to lengthen.     * Example: Tensed muscles such as a bicep curl; longitudinal pull/stretch of a ligament.
  • 2. Compressive Loading:     * Mechanism: Forces push into the tissue/body, "squishing" it toward the middle.     * Direction: Along the longitudinal axis and perpendicular to the analysis plane (transverse/frontal/sagittal).     * Action: Causes the body to shorten or deform.     * Example: Body weight pushing down on bone tissue.
  • 3. Shear Loading:     * Mechanism: Forces act parallel to each other but in opposite directions (material sliding past each other).     * Direction: Loading is applied medially-laterally; acts parallel to the analysis plane (perpendicular to frontal/sagittal, parallel to transverse).     * Example: The tibia sliding forward or backward relative to the femur.
  • 4. Torsion Loading:     * Mechanism: Due to torque applied on the longitudinal axis of the body at each end.     * Action: A rotational form of shear stress; twisting along the longitudinal line.     * Example: spine torsion when landing and upper body rotates while feet are fixed; walking creates torsion in the leg.
  • 5. Bending (Complex Loading):     * Mechanism: A combination of tensile and compressive stress within the same internal structure.     * Stress Profile: One side of the material experiences compression while the opposite side experiences tension.     * Real-world Example: Standing on a single leg puts 60% of body weight pushing down on the femoral head. Because the femur is stabilized, bending occurs on the neck of the femur.
  • 6. Combination Loading:     * A single bone may experience weight-bearing (compression), twisting (torsion), and muscle action (tension) simultaneously.

Stress and Strain Relationship

  • Strain (ϵ\epsilon):     * Definition: The measurement of deformation from the original length, often expressed as a percentage.     * Conceptual Distinction: Stress is the cause (load); strain is the effect (deformation).     * Formula:ϵ=lflili=Δlli\epsilon = \frac{l_f - l_i}{l_i} = \frac{\Delta l}{l_i}         \text{% Strain} = \frac{\Delta l}{l_i} \times 100     * Units: Dimensionless (ratio), but often expressed as decimal or percentage.
  • Stiffness and Young's Modulus:     * The slope of the stress-strain curve represents the stiffness of the material.     * Young's Modulus (EE):E=ΔσΔϵE = \frac{\Delta \sigma}{\Delta \epsilon}     * Interpretation: A steeper slope indicates a stiffer material (higher Young's Modulus). For example, it requires more stress to lengthen 10 rubber bands than one single band to the same distance; therefore, 10 bands have greater stiffness.

Stress-Strain Regions and Landmarks

  • Elastic Region: The area where the material deforms under stress but returns (recoils) to its original shape/length when the stress is removed.
  • Yield Point: The end of the linear elastic region. Stress beyond this point leads to the plastic region.
  • Plastic Region: The area where further stress results in permanent deformation. Even after stress is removed, the material will not return to its original length; it has a new shape.
  • Landmarks:     * Yield Strength: The stress level at the yield point; identifies the transition from elastic to plastic behavior.     * Ultimate Strength: The maximum stress a material is capable of withstanding before starting to fail.     * Failure Strength: The stress level at which the material ruptures or breaks (total rupture).
  • Toe Region: Seen in muscle-tendon units; a period of easy stretch where tissue is relaxed and does not require high levels of stress initially.

Toughness and Mechanical Energy

  • Definition: Toughness is the material's ability to absorb mechanical energy before breaking.
  • Measurement: Represented by the total area under the stress-strain curve (Combination of stress and strain capacity).
  • Verbatim Principles:     * Toughness is the capacity to do work (W=F×dW = F \times d).     * Brittle Materials: Can handle high stress but show minimal strain (deformation) before failure (e.g., dry bone, a sliding glass door). These are "strong but fragile" or not tough.     * Tough Materials: Can handle both high stress and high strain before failure (e.g., live bone vs. dry bone).

Composition of Connective Tissues

  • Constituents: Cell, Collagen, Elastin, Ground Substance, Mineral, Water.
  • Water Content by Tissue Type:     * Bone: 20% to 30% water (contains 45% mineral).     * Cartilage: 20% to 70% water.     * Tendon and Ligament: 25% to 70% water.

Viscoelasticity

  • Definition: Biological tissues are viscoelastic, meaning stress and strain behaviors depend on the rate and type of loading. Behaviors include:     * Creep: Under a constant compressive stress, strain increases over time as water is squeezed out of the tissue until strain reaches a maximum.     * Stress Relaxation: Under a constant compressive strain, stress initially increases as water is squeezed out, reaches a maximum, and then decreases (relaxes) to a lower value.     * Hysteresis: The phenomenon where the loading and unloading paths on a stress-strain curve are different. Energy is lost (usually as heat) during the cycle.
  • Mechanical properties across directions:     * Isotropic: Same mechanical properties in every direction.     * Anisotropic: Different mechanical properties in different directions (typical of biological tissues).

Specific Tissue Mechanics: Bone and Cartilage

  • Bone Categories:     * Cortical Bone: "Compact" bone; stiff; sustains roughly 2% of maximum strain before failure.     * Cancellous Bone: "Spongy" or trabecular bone; handles more deformation than cortical bone before breaking but has less overall strength.     * Ultimate Strength of Bone (Loading Modes):         * Compression: 200MPa200\,MPa         * Tension: 125MPa125\,MPa         * Shear: 65MPa65\,MPa     * Mechanical Reference: 1MPa=145lb/in21\,MPa = 145\,lb/in^2 (Transcript note suggests a variant of 125lb/in125\,lb/in as well).
  • Cartilage Structure:     * Composed of 70% water and 20% collagen fiber.     * Collagen Fiber Arrangement:         * Surface: Parallel to the surface.         * Middle: Randomly arranged.         * Deep (near bone): Perpendicular to the surface.

Tendon and Ligament Mechanics

  • Functional Goal: Ligaments connect bone-to-bone to stabilize the joint.
  • Typical Maximum Strain: Approximately 8-10%.
  • Stress-Strain Regions for Tendons/Ligaments:     1. Toe Region (Region 1): Physiological loading; slack is taken up.     2. Linear Region (Region 2): Consistent elastic behavior.     3. Partial Rupture (Region 3): Microfailures occur.     4. Complete Rupture (Region 4): Total failure/injury.

Practice Problems and Calculations

  • Ligament Strain Calculation:     * Given: Initial length (lil_i) = 1cm1\,cm; Final length (lfl_f) after loading = 1.001cm1.001\,cm.     * Calculation:ϵ=1.0011.01.0×100=0.1%\epsilon = \frac{1.001 - 1.0}{1.0} \times 100 = 0.1\%
  • Achilles Tendon Elongation:     * Given: Initial length = 10cm10\,cm; Strain = 6%6\%.     * Calculation:Δl=10cm×0.06=0.6cm\Delta l = 10\,cm \times 0.06 = 0.6\,cmlf=10.6cml_f = 10.6\,cm
  • Young's Modulus Calculation (from Graph Data):     * Given points: (X1,Y1)=(0.01,20)(X_1, Y_1) = (0.01, 20), (X2,Y2)=(0.02,40)(X_2, Y_2) = (0.02, 40).     * Formula:E=40200.020.01=200.01=2000kN/m/mE = \frac{40 - 20}{0.02 - 0.01} = \frac{20}{0.01} = 2000\,kN/m/m