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Stress Concentration at Bolt Hole (Mechanical & Civil Engineering) Solution

A structural engineer analyzes stress distribution around a circular bolt fastening hole in a structural steel gusset plate under heavy tensile loading. Geometric discontinuities cause severe localized stress risers that can initiate micro-cracking and brittle fatigue fracture.

From high-resolution Finite Element Analysis (FEA) simulation, the Von Mises mechanical stress σ(x,y)\sigma(x, y) (in megapascals, MPa\text{MPa}) near the bolt hole boundary is described by:

σ(x,y)=400x2+2y2+1\sigma(x, y) = \frac{400}{x^2 + 2y^2 + 1}
where xx and yy represent planar spatial coordinates in millimeters (mm\text{mm}) measured from the center of the fastening aperture.

  1. State the Quotient Rule and Reciprocal Power Rule representations used to compute ∂σ∂x\frac{\partial \sigma}{\partial x} and ∂σ∂y\frac{\partial \sigma}{\partial y}.
  2. Determine general algebraic expressions for the spatial stress gradients ∂σ∂x\frac{\partial \sigma}{\partial x} and ∂σ∂y\frac{\partial \sigma}{\partial y}.
  3. Evaluate the instantaneous stress gradients at the critical monitoring coordinate (x,y)=(1,1) mm(x, y) = (1, 1)\text{ mm}.
  4. State the physical units of these derivatives. Geometrically interpret what these values mean if an inspector moves away from the bolt hole along the +x+x vs +y+y directions.

Step-by-Step Solution:

  1. State the Differentiation Rules:

    • Writing σ(x,y)=400(x2+2y2+1)−1\sigma(x, y) = 400(x^2 + 2y^2 + 1)^{-1}, apply the Generalized Power Chain Rule:
      ∂∂x[c⋅u−1]=−c⋅u−2⋅∂u∂x=−cu2∂u∂x\frac{\partial}{\partial x}[c \cdot u^{-1}] = -c \cdot u^{-2} \cdot \frac{\partial u}{\partial x} = -\frac{c}{u^2} \frac{\partial u}{\partial x}
      (Defined in Partial Derivatives and Geometric Interpretation of Partial Derivatives.)
  2. Compute the General Algebraic Expressions:

    • Let u(x,y)=x2+2y2+1u(x, y) = x^2 + 2y^2 + 1.
    • Differentiating with respect to xx (holding yy constant):
      ∂u∂x=2x\frac{\partial u}{\partial x} = 2x
      ∂σ∂x=−400(x2+2y2+1)2⋅(2x)=−800x(x2+2y2+1)2\frac{\partial \sigma}{\partial x} = -\frac{400}{(x^2 + 2y^2 + 1)^2} \cdot (2x) = -\frac{800x}{(x^2 + 2y^2 + 1)^2}
    • Differentiating with respect to yy (holding xx constant):
      ∂u∂y=4y\frac{\partial u}{\partial y} = 4y
      ∂σ∂y=−400(x2+2y2+1)2⋅(4y)=−1600y(x2+2y2+1)2\frac{\partial \sigma}{\partial y} = -\frac{400}{(x^2 + 2y^2 + 1)^2} \cdot (4y) = -\frac{1600y}{(x^2 + 2y^2 + 1)^2}
  3. Evaluate at the Point (1,1) mm(1, 1)\text{ mm}:

    • Evaluate denominator u(1,1)u(1, 1):
      u(1,1)=12+2(1)2+1=1+2+1=4u(1, 1) = 1^2 + 2(1)^2 + 1 = 1 + 2 + 1 = 4
      u2=42=16u^2 = 4^2 = 16
    • Evaluate ∂σ∂x(1,1)\frac{\partial \sigma}{\partial x}(1, 1):
      ∂σ∂x∣(1,1)=−800(1)16=−50 MPa/mm\left.\frac{\partial \sigma}{\partial x}\right|_{(1, 1)} = -\frac{800(1)}{16} = -50\text{ MPa/mm}
    • Evaluate ∂σ∂y(1,1)\frac{\partial \sigma}{\partial y}(1, 1):
      ∂σ∂y∣(1,1)=−1600(1)16=−100 MPa/mm\left.\frac{\partial \sigma}{\partial y}\right|_{(1, 1)} = -\frac{1600(1)}{16} = -100\text{ MPa/mm}
  4. Physical Units and Geometric Interpretation:

    • Units: Megapascals per millimeter (MPa/mm\text{MPa/mm}).
    • Geometric Interpretation: At (1,1)(1, 1), moving in the positive xx-direction (holding y=1 mmy = 1\text{ mm}) causes localized stress to drop at an instantaneous rate of 50 MPa/mm50\text{ MPa/mm}. Moving in the positive yy-direction (holding x=1 mmx = 1\text{ mm}) causes stress to plunge twice as rapidly, at −100 MPa/mm-100\text{ MPa/mm}.
    • Engineering Consequence: The stress gradient is significantly steeper along the yy-axis because of the coefficient 22 in the ellipse geometry. Crack initiation risk diminishes twice as rapidly as you step along yy away from the notch than along xx.