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Derive the Bernoulli equation when the compressibility eff undergoing: a. An isothermal process, and b. An isentropic process

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2 parts
a

RTln⁡P+V22+gz=constantRT \ln P + \frac{V^2}{2} + gz = \text{constant}

b

kk−1Pρ+V22+gz=constant\frac{k}{k-1} \frac{P}{\rho} + \frac{V^2}{2} + gz = \text{constant}

Step-by-step solution

10 steps

The Bernoulli equation for a compressible fluid is derived from the Euler equation for steady, inviscid flow along a streamline:

dPρ+VdV+gdz=0\frac{dP}{\rho} + V dV + g dz = 0

Integrating this equation yields the Bernoulli equation. The form of the pressure integral ∫dPρ\int \frac{dP}{\rho} depends on the thermodynamic process.

Part a· 5 steps

An isothermal process

  1. Start with the Euler equation.

    dPρ+VdV+gdz=0\frac{dP}{\rho} + V dV + g dz = 0
  2. Apply the condition for an isothermal process for an ideal gas.

    For an isothermal process, the temperature TT is constant.
    The ideal gas law is P=ρRTP = \rho R T.
    From this, we can express density ρ\rho in terms of pressure PP:

    ρ=PRT\rho = \frac{P}{RT}

    Since RR (gas constant) and TT (temperature) are constant, RTRT is a constant.

  3. Substitute the expression for ρ\rho into the Euler equation.

    dP(P/RT)+VdV+gdz=0\frac{dP}{(P/RT)} + V dV + g dz = 0 RTdPP+VdV+gdz=0RT \frac{dP}{P} + V dV + g dz = 0
  4. Integrate the equation.

    Integrate each term along a streamline from an initial point to a final point:

    ∫RTdPP+∫VdV+∫gdz=constant\int RT \frac{dP}{P} + \int V dV + \int g dz = \text{constant} RTln⁡P+V22+gz=constantRT \ln P + \frac{V^2}{2} + gz = \text{constant}
  5. State the Bernoulli equation for an isothermal process.

    The Bernoulli equation for a compressible fluid undergoing an isothermal process is:

    RTln⁡P+V22+gz=constant\boxed{RT \ln P + \frac{V^2}{2} + gz = \text{constant}}

Part b

kk−1Pρ+V22+gz=constant\frac{k}{k-1} \frac{P}{\rho} + \frac{V^2}{2} + gz = \text{constant}

An isentropic process

  1. Start with the Euler equation.

    dPρ+VdV+gdz=0\frac{dP}{\rho} + V dV + g dz = 0
  2. Apply the condition for an isentropic process for an ideal gas.

    For an isentropic process (adiabatic and reversible), the relationship between pressure PP and density ρ\rho for an ideal gas is:

    Pρk=C\frac{P}{\rho^k} = C

    where CC is a constant and k=cpcvk = \frac{c_p}{c_v} is the ratio of specific heats.
    From this, we can express 1ρ\frac{1}{\rho} in terms of PP:

    ρ=(PC)1/k  ⟹  1ρ=C1/kP−1/k\rho = \left(\frac{P}{C}\right)^{1/k} \implies \frac{1}{\rho} = C^{1/k} P^{-1/k}
  3. Substitute the expression for 1ρ\frac{1}{\rho} into the Euler equation.

    C1/kP−1/kdP+VdV+gdz=0C^{1/k} P^{-1/k} dP + V dV + g dz = 0
  4. Integrate the equation.

    Integrate each term along a streamline:

    ∫C1/kP−1/kdP+∫VdV+∫gdz=constant\int C^{1/k} P^{-1/k} dP + \int V dV + \int g dz = \text{constant}

    Let's evaluate the pressure integral:

    ∫C1/kP−1/kdP=C1/kP(−1/k)+1(−1/k)+1=C1/kP(k−1)/k(k−1)/k=kk−1C1/kP(k−1)/k\int C^{1/k} P^{-1/k} dP = C^{1/k} \frac{P^{(-1/k)+1}}{(-1/k)+1} = C^{1/k} \frac{P^{(k-1)/k}}{(k-1)/k} = \frac{k}{k-1} C^{1/k} P^{(k-1)/k}

    Now, substitute C1/k=P1/kρC^{1/k} = \frac{P^{1/k}}{\rho}:

    kk−1(P1/kρ)P(k−1)/k=kk−1P1/k+(k−1)/kρ=kk−1Pk/kρ=kk−1Pρ\frac{k}{k-1} \left(\frac{P^{1/k}}{\rho}\right) P^{(k-1)/k} = \frac{k}{k-1} \frac{P^{1/k + (k-1)/k}}{\rho} = \frac{k}{k-1} \frac{P^{k/k}}{\rho} = \frac{k}{k-1} \frac{P}{\rho}

    So, the integrated pressure term is kk−1Pρ\frac{k}{k-1} \frac{P}{\rho}.

  5. State the Bernoulli equation for an isentropic process.

    The Bernoulli equation for a compressible fluid undergoing an isentropic process is:

    kk−1Pρ+V22+gz=constant\boxed{\frac{k}{k-1} \frac{P}{\rho} + \frac{V^2}{2} + gz = \text{constant}}
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