Fluid Mechanics and Hydraulic Machinery Miscellaneous


Fluid Mechanics and Hydraulic Machinery Miscellaneous

Fluid Mechanics and Hydraulic Machinery

  1. A water container is kept on a weighing balance. Water from a tap is falling vertically into the container with a volume flow rate of Q; the velocity of the water when it hits the water surface is U. At a particular instant of time the total mass of the container and water is m. The force registered by the weighing balance at this instant of time is









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    Volume flow rate = Q
    Mass of water strike = ρQ
    Velocity of the water when it hit the water surface = U
    Force on weighing balance due to water strike = Initial momentum – final momentum
    = ρQU – 0= ρQU
    (since final velocity is perpendicular to initial velocity)
    Now total force on weighing balance = mg + ρQU

    Correct Option: A

    Volume flow rate = Q
    Mass of water strike = ρQ
    Velocity of the water when it hit the water surface = U
    Force on weighing balance due to water strike = Initial momentum – final momentum
    = ρQU – 0= ρQU
    (since final velocity is perpendicular to initial velocity)
    Now total force on weighing balance = mg + ρQU


  1. A fan in the duct shown below sucks air from the ambient and expels it as a jet at 1 m/s to the ambient. Determine the gauge pressure at the point marked as A. Take the density of air as 1 kg/m3.









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    Applying Bernoulli’s equation between sections (i) & A

    P1 =
    PA
    +
    VA²
    ρg2g

    PA - P1
    =
    -VA²
    ρg2g

    P1 = Pambient
    ∴ PA - P1 = (PA)gauge
    (PA)gauge
    ==
    -VA²
    ρg2g

    (PA)gauge =
    -1 × 1²
    = 0.5N/m²
    2

    Correct Option: A

    Applying Bernoulli’s equation between sections (i) & A

    P1 =
    PA
    +
    VA²
    ρg2g

    PA - P1
    =
    -VA²
    ρg2g

    P1 = Pambient
    ∴ PA - P1 = (PA)gauge
    (PA)gauge
    ==
    -VA²
    ρg2g

    (PA)gauge =
    -1 × 1²
    = 0.5N/m²
    2



  1. A two-dimensional incompressible frictionless flow field is given by μ = xi - yj. If ρ is the density of the fluid, the expression for pressure gradient vector at any point in the flow field is given as









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    NA

    Correct Option: D

    NA


  1. For a steady flow, the velocity field is V = (–x² + 3y) i + (2xy)j. The magnitude of the acceleration of a particle at (1, - 1) is









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    NA

    Correct Option: C

    NA



  1. For a two-dimensional flow, the velocity field is
    u =
    x
    i +
    y
    j
    x² + y²x² + y²

    where i and j are the basis vectors in the x – y Cartesian coordinate system. Identify the CORRECT statements from below.
    1. The flow is incompressible
    2. The flow is unsteady
    3. y-component of acceleration,
    ay =
    - y
    (x² + y²)²

    4. x-component of acceleration,
    ax =
    -(x + y)
    (x² + y²)²









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    axu
    δu
    + v
    δu
    δxδy


    =
    x(x² + y² -2x²)-2xy²
    =
    - x3 - xy²
    (x² + y²)(x² + y²)(x² + y²)

    ∴ ax =
    x
    (x² + y²)²

    ay = u
    δv
    + v
    δv
    δxδy


    =
    -x² + yx² - y3
    =
    - y
    (x² + y²)3(x² + y²)²

    The velocity components are not functions of time, so flow is steady according to continuity equation,

    Since it satisfies the above continuity equation for 2D and incompressible flow.
    ∴ The flow is incompressible.

    Correct Option: B

    axu
    δu
    + v
    δu
    δxδy


    =
    x(x² + y² -2x²)-2xy²
    =
    - x3 - xy²
    (x² + y²)(x² + y²)(x² + y²)

    ∴ ax =
    x
    (x² + y²)²

    ay = u
    δv
    + v
    δv
    δxδy


    =
    -x² + yx² - y3
    =
    - y
    (x² + y²)3(x² + y²)²

    The velocity components are not functions of time, so flow is steady according to continuity equation,

    Since it satisfies the above continuity equation for 2D and incompressible flow.
    ∴ The flow is incompressible.