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Question

The only possible dimensionless group that combines velocity ‘V’, body size ‘L’, fluid density ‘ρ’ & surface tension ‘σ’

The correct answer is \(\frac {\rho L V^2}{\sigma}\)

Dimensional Analysis for Fluid Mechanics Parameters

In fluid mechanics, understanding the relationships between different physical quantities is crucial. Dimensional analysis is a powerful tool used to derive relationships among physical quantities and to group them into dimensionless parameters. These dimensionless groups are essential for scaling experimental results and for theoretical modeling, ensuring that experimental findings can be applied to real-world scenarios regardless of scale.

Understanding Parameter Dimensions

To form a dimensionless group, we first need to determine the fundamental dimensions of each given physical quantity: velocity (\(V\)), body size (\(L\)), fluid density (\(\rho\)), and surface tension (\(\sigma\)). The fundamental dimensions used are Mass (\(M\)), Length (\(L\)), and Time (\(T\)).

Parameter Symbol Dimensions Common Units
Velocity \(V\) \([LT^{-1}]\) meters per second (m/s)
Body Size (Characteristic Length) \(L\) \([L]\) meters (m)
Fluid Density \(\rho\) \([ML^{-3}]\) kilograms per cubic meter (kg/m3)
Surface Tension \(\sigma\) \([MT^{-2}]\) Newtons per meter (N/m) or kilograms per square second (kg/s2)

Dimensionless Group Derivation

We are looking for a dimensionless group, often denoted as \(\Pi\), that combines these four variables. A dimensionless group has no physical units, meaning its dimensions are \([M^0 L^0 T^0]\). We can express this group as a product of the variables raised to some unknown powers:

\(\Pi = V^a L^b \rho^c \sigma^d\)

Now, we substitute the dimensions of each variable into the equation:

\([M^0 L^0 T^0] = ([LT^{-1}])^a ([L])^b ([ML^{-3}])^c ([MT^{-2}])^d\)

Next, we collect the powers of \(M\), \(L\), and \(T\) on the right-hand side of the equation:

  • For Mass (\(M\)): The total power of \(M\) is \(c\) (from \(\rho\)) + \(d\) (from \(\sigma\)).
  • For Length (\(L\)): The total power of \(L\) is \(a\) (from \(V\)) + \(b\) (from \(L\)) - \(3c\) (from \(\rho\)).
  • For Time (\(T\)): The total power of \(T\) is \(-a\) (from \(V\)) - \(2d\) (from \(\sigma\)).

To ensure \(\Pi\) is dimensionless, we must equate the sum of the powers of each fundamental dimension to zero:

  1. For M: \(c + d = 0 \implies c = -d\)
  2. For L: \(a + b - 3c = 0\)
  3. For T: \(-a - 2d = 0 \implies a = -2d\)

We have a system of 3 linear equations with 4 unknowns (\(a, b, c, d\)). This means we can express three exponents in terms of the fourth, or we can choose one exponent arbitrarily. Let's choose \(d = -1\). This choice often places the surface tension in the denominator, which is characteristic of many dimensionless numbers involving surface tension effects.

  • From equation (1): \(c = -(-1) = 1\)
  • From equation (3): \(a = -2(-1) = 2\)
  • Now, substitute the values of \(a=2\) and \(c=1\) into equation (2):
    \(2 + b - 3(1) = 0\)
    \(2 + b - 3 = 0\)
    \(b - 1 = 0\)
    \(b = 1\)

So, the exponents for our variables are \(a=2\), \(b=1\), \(c=1\), and \(d=-1\).

Substituting these values back into the expression for \(\Pi\):

\(\Pi = V^2 L^1 \rho^1 \sigma^{-1} = \frac{\rho V^2 L}{\sigma}\)

This particular dimensionless group is famously known as the Weber Number (We). It is a crucial parameter in fluid dynamics, especially for flows where there is an interface between two different fluids (like liquid-gas interfaces). The Weber Number represents the ratio of inertial forces to surface tension forces, and it helps predict the onset of phenomena such as droplet breakup or bubble formation.

Comparing with Given Options

Let's compare our meticulously derived dimensionless group with the provided options to identify the correct choice:

  • Option 1: \(\frac {L\rho \sigma}{V}\)
  • Option 2: \(\frac {\rho VL^2}{\sigma}\)
  • Option 3: \(\frac {\sigma L V^2}{\rho}\)
  • Option 4: \(\frac {\rho L V^2}{\sigma}\)

Our derived group, \(\frac{\rho V^2 L}{\sigma}\), is identical to Option 4, which is presented as \(\frac{\rho L V^2}{\sigma}\). The order of multiplication in the numerator does not change the value of the term.

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Important Questions from Dimensionless Number

  1. Match the following and select the correct answer from the codes given below the lists

    List I

    List II

    A.

    Steam Nozzle

    1.

    Mach number

    B.

    Compressible flow

    2.

    Reaction turbine

    C.

    Surface Tension

    3.

    Biot number

    D.

    Heat conduction

    4.

    Nusselt number

    5.

    Supersaturation

    6.

    Weber number

  2. The Reynold’s number, used for critical velocity for turbulent flow of fluids, is given by the relation

  3. Reynolds number for non - circular cross-section is:

    [V = mean velocity, ν = kinematic viscosity, P = ratio of cross-sectional area to the wetted perimeter]

    A) \(V.\frac{{4P}}{v}\)

    B) \(\frac{{V.P}}{v}\)

    C) \(\frac{{V.2P}}{{4v}}\)

    D) \(\frac{{V.P}}{{4v}}\)

  4. When the Mach number is less than unity, the flow is

  5. Which of the following is not a non-dimensional parameter?
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