Math Problem Statement

a thin walled cylinder with closed ends has id 1m & od 1.04m . this cylinder is subjected to internal pressure 4mpa . what will be the absolute maximum shear stress on inner surface

Solution

To determine the absolute maximum shear stress on the inner surface of the thin-walled cylinder, we follow these steps:


Step 1: Assumptions

The cylinder has thin walls. For a thin-walled pressure vessel, the radial stress is negligible compared to the hoop (circumferential) and axial stresses.

Step 2: Dimensions and Parameters

  • Internal diameter, din=1md_{\text{in}} = 1\, \text{m}
  • Outer diameter, dout=1.04md_{\text{out}} = 1.04\, \text{m}
  • Wall thickness, t=doutdin2=1.0412=0.02mt = \frac{d_{\text{out}} - d_{\text{in}}}{2} = \frac{1.04 - 1}{2} = 0.02\, \text{m}
  • Internal pressure, p=4MPap = 4\, \text{MPa}

Step 3: Thin-Walled Cylinder Stress Analysis

(a) Hoop Stress (σh\sigma_h):

σh=print\sigma_h = \frac{p \cdot r_{\text{in}}}{t} Where rinr_{\text{in}} is the inner radius of the cylinder: rin=din2=12=0.5mr_{\text{in}} = \frac{d_{\text{in}}}{2} = \frac{1}{2} = 0.5\, \text{m} Substitute values: σh=4×1060.50.02=100×106=100MPa\sigma_h = \frac{4 \times 10^6 \cdot 0.5}{0.02} = 100 \times 10^6 = 100\, \text{MPa}

(b) Axial Stress (σa\sigma_a):

σa=prin2t\sigma_a = \frac{p \cdot r_{\text{in}}}{2t} Substitute values: σa=4×1060.520.02=50×106=50MPa\sigma_a = \frac{4 \times 10^6 \cdot 0.5}{2 \cdot 0.02} = 50 \times 10^6 = 50\, \text{MPa}


Step 4: Maximum Shear Stress on Inner Surface

The maximum shear stress is calculated using the formula: τmax=σhσa2\tau_{\text{max}} = \frac{\sigma_h - \sigma_a}{2} Substitute the hoop and axial stresses: τmax=100502=25MPa\tau_{\text{max}} = \frac{100 - 50}{2} = 25\, \text{MPa}


Final Answer

The absolute maximum shear stress on the inner surface is: 25MPa\boxed{25\, \text{MPa}}


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Further Questions

  1. What is the formula for maximum shear stress in a thick-walled cylinder?
  2. How does the stress distribution differ in thin vs. thick-walled pressure vessels?
  3. Can we calculate radial stress for this thin-walled cylinder?
  4. What assumptions make thin-wall theory applicable here?
  5. What are common materials used for cylinders under high internal pressure?

Tip

Always validate the thin-wall assumption by ensuring trint \ll r_{\text{in}}. For this case, t/rin=0.02/0.5=0.04t / r_{\text{in}} = 0.02 / 0.5 = 0.04, which is valid.

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Math Problem Analysis

Mathematical Concepts

Mechanics of Materials
Stress Analysis
Thin-Walled Pressure Vessels

Formulas

Hoop stress: σ_h = (p * r_in) / t
Axial stress: σ_a = (p * r_in) / (2 * t)
Maximum shear stress: τ_max = (σ_h - σ_a) / 2

Theorems

Stress distribution in thin-walled cylinders
Shear stress calculation for pressure vessels

Suitable Grade Level

Undergraduate Engineering (Year 2-3)