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Using Buckingham's Pi Theorem, determine the functional relationship for the resistance of a supersonic plane.

Physics

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To determine the functional relationship for the resistance (R) of a supersonic plane using Buckingham's Pi Theorem, we follow these steps:

  1. List all variables and their dimensions.

    The variables involved are:

    • Resistance, RR (Force)
    • Aircraft Length, LL
    • Velocity, VV
    • Air Viscosity, μ\mu (Dynamic Viscosity)
    • Air Density, ρ\rho
    • Bulk Modulus, KK (Pressure)

    Their fundamental dimensions (in terms of Mass [M], Length [L], Time [T]) are:

    • R=[MLT−2]R = [M L T^{-2}]
    • L=[L]L = [L]
    • V=[LT−1]V = [L T^{-1}]
    • μ=[ML−1T−1]\mu = [M L^{-1} T^{-1}]
    • ρ=[ML−3]\rho = [M L^{-3}]
    • K=[ML−1T−2]K = [M L^{-1} T^{-2}]
  2. Determine the number of variables (nn) and fundamental dimensions (mm).

    • Number of variables, n=6n = 6
    • Number of fundamental dimensions, m=3m = 3 (M, L, T)
  3. Calculate the number of dimensionless Π\Pi groups.

    According to Buckingham's Pi Theorem, the number of dimensionless groups is n−m=6−3=3n - m = 6 - 3 = 3.

  4. Select repeating variables.

    We need to choose m=3m=3 repeating variables that collectively contain all fundamental dimensions (M, L, T) and do not form a dimensionless group among themselves. A common and suitable choice for fluid dynamics problems is:

    • Density, ρ=[ML−3]\rho = [M L^{-3}]
    • Velocity, V=[LT−1]V = [L T^{-1}]
    • Length, L=[L]L = [L]
  5. Form the dimensionless Π\Pi groups.

    Each Π\Pi group is formed by combining a non-repeating variable with the repeating variables raised to unknown powers (a,b,ca, b, c):
    Πi=(non-repeating variable)×ρaVbLc\Pi_i = (\text{non-repeating variable}) \times \rho^a V^b L^c

    Π1\Pi_1 (using Resistance, RR):

    Π1=RρaVbLc\Pi_1 = R \rho^a V^b L^c

    Substitute dimensions:

    [M0L0T0]=[MLT−2][ML−3]a[LT−1]b[L]c[M^0 L^0 T^0] = [M L T^{-2}] [M L^{-3}]^a [L T^{-1}]^b [L]^c [M0L0T0]=[M1+aL1−3a+b+cT−2−b][M^0 L^0 T^0] = [M^{1+a} L^{1-3a+b+c} T^{-2-b}]

    Equating powers for M, L, T:

    • For M: 1+a=0  ⟹  a=−11 + a = 0 \implies a = -1
    • For T: −2−b=0  ⟹  b=−2-2 - b = 0 \implies b = -2
    • For L: 1−3a+b+c=0  ⟹  1−3(−1)+(−2)+c=0  ⟹  1+3−2+c=0  ⟹  2+c=0  ⟹  c=−21 - 3a + b + c = 0 \implies 1 - 3(-1) + (-2) + c = 0 \implies 1 + 3 - 2 + c = 0 \implies 2 + c = 0 \implies c = -2 Therefore,
    Π1=Rρ−1V−2L−2=RρV2L2\Pi_1 = R \rho^{-1} V^{-2} L^{-2} = \frac{R}{\rho V^2 L^2}

    Π2\Pi_2 (using Air Viscosity, μ\mu):

    Π2=μρaVbLc\Pi_2 = \mu \rho^a V^b L^c

    Substitute dimensions:

    [M0L0T0]=[ML−1T−1][ML−3]a[LT−1]b[L]c[M^0 L^0 T^0] = [M L^{-1} T^{-1}] [M L^{-3}]^a [L T^{-1}]^b [L]^c [M0L0T0]=[M1+aL−1−3a+b+cT−1−b][M^0 L^0 T^0] = [M^{1+a} L^{-1-3a+b+c} T^{-1-b}]

    Equating powers for M, L, T:

    • For M: 1+a=0  ⟹  a=−11 + a = 0 \implies a = -1
    • For T: −1−b=0  ⟹  b=−1-1 - b = 0 \implies b = -1
    • For L: −1−3a+b+c=0  ⟹  −1−3(−1)+(−1)+c=0  ⟹  −1+3−1+c=0  ⟹  1+c=0  ⟹  c=−1-1 - 3a + b + c = 0 \implies -1 - 3(-1) + (-1) + c = 0 \implies -1 + 3 - 1 + c = 0 \implies 1 + c = 0 \implies c = -1 Therefore,
    Π2=μρ−1V−1L−1=μρVL\Pi_2 = \mu \rho^{-1} V^{-1} L^{-1} = \frac{\mu}{\rho V L}

    (This is the inverse of the Reynolds number, Re=ρVLμRe = \frac{\rho V L}{\mu})

    Π3\Pi_3 (using Bulk Modulus, KK):

    Π3=KρaVbLc\Pi_3 = K \rho^a V^b L^c

    Substitute dimensions:

    [M0L0T0]=[ML−1T−2][ML−3]a[LT−1]b[L]c[M^0 L^0 T^0] = [M L^{-1} T^{-2}] [M L^{-3}]^a [L T^{-1}]^b [L]^c [M0L0T0]=[M1+aL−1−3a+b+cT−2−b][M^0 L^0 T^0] = [M^{1+a} L^{-1-3a+b+c} T^{-2-b}]

    Equating powers for M, L, T:

    • For M: 1+a=0  ⟹  a=−11 + a = 0 \implies a = -1
    • For T: −2−b=0  ⟹  b=−2-2 - b = 0 \implies b = -2
    • For L: $-1 - 3a + b + c = 0 \implies -1 - 3(-1) + (-2) + c = 0 \implies -1 + 3 - 2 + c =
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