A rectangular mine airway of 2.0 m width and 2.5 m height has a bend with deflection of π/4 radian. If the radius of curvature of the bend is 4.0 m, the shock factor of the bend is... A rectangular mine airway of 2.0 m width and 2.5 m height has a bend with deflection of π/4 radian. If the radius of curvature of the bend is 4.0 m, the shock factor of the bend is (round off to three decimals)

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Understand the Problem

The question is asking us to calculate the shock factor of a bend in a mine airway, given its dimensions and the radius of curvature. This involves applying principles of fluid mechanics to find the required value.

Answer

The shock factor of the bend is \( 0.014 \).
Answer for screen readers

The shock factor of the bend is approximately ( 0.014 ).

Steps to Solve

  1. Identify the dimensions and parameters
    The dimensions of the rectangular airway are:

    • Width ( W = 2.0 , \text{m} )
    • Height ( H = 2.5 , \text{m} )
      The bend has a radius of curvature ( R = 4.0 , \text{m} ) and a deflection angle ( \theta = \frac{\pi}{4} , \text{radians} ).
  2. Calculate the cross-sectional area of the airway
    The cross-sectional area ( A ) can be calculated as:
    $$ A = W \times H = 2.0 , \text{m} \times 2.5 , \text{m} = 5.0 , \text{m}^2 $$

  3. Find the hydraulic radius (R_h)
    The hydraulic radius for a rectangular section can be calculated as:
    $$ R_h = \frac{A}{P} $$
    The wetted perimeter ( P ) for a rectangular channel is defined as:
    $$ P = W + 2H = 2.0 , \text{m} + 2 \times 2.5 , \text{m} = 7.0 , \text{m} $$
    Now, substituting the values:
    $$ R_h = \frac{5.0 , \text{m}^2}{7.0 , \text{m}} \approx 0.7142857142857143 , \text{m} $$

  4. Calculate the shock factor (S)
    The shock factor can be calculated using the formula:
    $$ S = \frac{R_h}{R} \cdot \theta $$
    Substituting the values gives:
    $$ S = \frac{0.7142857142857143 , \text{m}}{4.0 , \text{m}} \cdot \frac{\pi}{4} $$
    $$ S \approx \frac{0.7142857142857143}{4.0} \cdot 0.7853981633974483 $$
    $$ S \approx 0.014 , (\text{approx}) $$

  5. Round the answer
    The final calculated shock factor should be rounded to three decimal places, which is:
    $$ S \approx 0.014 $$

The shock factor of the bend is approximately ( 0.014 ).

More Information

The shock factor is a measure used in fluid mechanics to determine the effects of a bend in a channel on the flow of fluid. It considers both the geometry of the channel and the properties of the fluid.

Tips

  • Confusing the wetted perimeter with the overall dimensions of the channel. Always ensure the correct interpretation of which edges contribute to the wetted perimeter.
  • Failing to convert units appropriately if necessary; however, in this case, all measurements were already in meters.

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