Math Problem Statement

A long, thick-walled cylinder made of steel (E = 200 GPa, ν = 0.3, a = 2 cm, b = 4 cm) encloses a rigid solid cylinder. It is subjected to an external pressure p₀ = 200 MPa. Required: a. State the boundary conditions (BCs). b. Determine and draw the stress distributions (σᵣᵣ(r) and σₜₜ(r)) in the steel cylinder.

Solution

Solution for Problem 4:

We are tasked with solving the problem of a thick-walled cylinder under external pressure p0=200MPap_0 = 200 \, \text{MPa}. The key parameters given are:

  • Material of the cylinder: Steel (E=200GPa,ν=0.3E = 200 \, \text{GPa}, \nu = 0.3)
  • Cylinder inner radius: a=2cma = 2 \, \text{cm}
  • Cylinder outer radius: b=4cmb = 4 \, \text{cm}
  • The cylinder encloses a rigid solid core (gray), which will impose specific boundary conditions.

Part (a): State the Boundary Conditions (BCs)

The boundary conditions (BCs) for the problem are determined based on the physical constraints:

  1. Inner boundary (r=ar = a): The rigid solid cylinder (gray) does not deform, meaning: u(a) = 0 \quad \text{(no radial displacement at r = a)}.

  2. Outer boundary (r=br = b): The external pressure p0=200MPap_0 = 200 \, \text{MPa} acts uniformly on the outer surface of the cylinder. The radial stress at the outer boundary is: \sigma_{rr}(b) = -p_0 \quad \text{(compressive radial stress at r = b)}.

  3. Negligible body forces: There are no body forces acting in the cylinder, so fr=0f_r = 0.


Part (b): Stress Distributions (σrr(r),σθθ(r))(\sigma_{rr}(r), \sigma_{\theta\theta}(r))

For a thick-walled cylinder under external pressure, the stress distribution can be solved using Lame's Equations in elasticity. The stress components in cylindrical coordinates are:

Radial Stress (σrr(r)\sigma_{rr}(r)):

σrr(r)=ABr2\sigma_{rr}(r) = A - \frac{B}{r^2}

Hoop (Circumferential) Stress (σθθ(r)\sigma_{\theta\theta}(r)):

σθθ(r)=A+Br2\sigma_{\theta\theta}(r) = A + \frac{B}{r^2}

Here, AA and BB are constants determined by the boundary conditions.


Step 1: Apply BCs to Find Constants AA and BB

  1. At r=ar = a: u(a)=0u(a) = 0
    The radial displacement u(r)u(r) is given by: u(r)=1E[(1+ν)σθθ(r)νσrr(r)]r.u(r) = \frac{1}{E} \left[ (1+\nu) \sigma_{\theta\theta}(r) - \nu \sigma_{rr}(r) \right] \cdot r. Substituting σrr(r)\sigma_{rr}(r) and σθθ(r)\sigma_{\theta\theta}(r) into u(a)=0u(a) = 0 will relate AA and BB.

  2. At r=br = b: σrr(b)=p0\sigma_{rr}(b) = -p_0
    Substitute r=br = b into σrr(r)\sigma_{rr}(r): p0=ABb2.-p_0 = A - \frac{B}{b^2}.


Step 2: Solve for Stress Distributions

Using the above conditions, solve for AA and BB. After determining AA and BB, substitute them back into σrr(r)\sigma_{rr}(r) and σθθ(r)\sigma_{\theta\theta}(r) to obtain the stress distributions as functions of rr.


Step 3: Draw the Stress Distributions

Once σrr(r)\sigma_{rr}(r) and σθθ(r)\sigma_{\theta\theta}(r) are computed, plot the stress components as a function of rr from a=2cma = 2 \, \text{cm} to b=4cmb = 4 \, \text{cm}. The radial stress will decrease from the applied external pressure at r=br = b, while the hoop stress will vary across the cylinder wall.


Would you like detailed computations of constants AA and BB, and the stress distribution equations?


Related Questions

  1. How do the material properties (E,νE, \nu) affect the stress distribution in the cylinder?
  2. How would the problem change if the external pressure p0p_0 was replaced by an internal pressure pip_i?
  3. Can you derive the displacement equation u(r)u(r) in detail for this problem?
  4. What are the maximum and minimum stresses in the cylinder, and where do they occur?
  5. How would the solution change if the gray core were elastic instead of rigid?

Tip

Always double-check the boundary conditions when solving elasticity problems, as they are crucial for accurately determining stress and displacement distributions.

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Math Problem Analysis

Mathematical Concepts

Elasticity
Stress Analysis
Boundary Conditions

Formulas

σᵣᵣ(r) = A - B/r²
σₜₜ(r) = A + B/r²
u(r) = (1/E) * [(1 + ν)σₜₜ(r) - νσᵣᵣ(r)] * r

Theorems

Lame's Equations

Suitable Grade Level

University Level (Mechanical/Civil Engineering)