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QUIZ-1-Fluid-Machineries

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QUIZ 1
At the pressure side of the compressor 2.5 bar absolute
pressure and 187°C temperature was measured, the
temperature of the inflow air is 27°C, and the pressure
at the suction side is 1020 hPa (1 hPa = 100Pa). Find
the polytropic exponent of the compression and the
polytropic efficiency of the process, if k = 1.4! (Solution:
n = 1:911, npol = 0.6).
Solution:
𝑛−1
𝑛
𝑇2
𝑃2
=( )
𝑇1
𝑃1
4. Ideal gas (gas constant R = 288 J/kgK, specific heat
at constant pressure is cp = 1005 J/kgK) with 27°C and
1 bar pressure is compressed to 3 bar with compressor.
The exponent describing the real state of change is n =
1.5. Find the absolute temperature and density of the
air at the outlet. Find the isentropic outlet temperature,
the isentropic efficiency and the isentropic useful
specific work if the mass ow is 3 kg/s. (Solution: Treal =
432.7K, 𝜌 = 2.407 kg/m3, Tisentropic = 410.6K, πœ‚ isentropic =
83.3%, Yisentropic = 111.48 kJ/kg)
Solution:
𝑛−1
𝑛
460𝐾
2.5 π‘π‘Žπ‘Ÿ
=(
)
300𝐾
1.02 π‘π‘Žπ‘Ÿ
𝒏 = 𝟏. πŸ—πŸπŸ
𝑛
π‘˜−1
(
)
𝑛−1
π‘˜
1.911
1.4 − 1
πœ‚π‘π‘œπ‘™π‘¦ =
(
)
1.911 − 1
1.4
πœΌπ’‘π’π’π’š = 𝟎. πŸ” 𝒐𝒓 πŸ”πŸŽ%
πœ‚π‘π‘œπ‘™π‘¦ =
2. A 1 m3 rigid tank initially contains air whose density
is 1.18kg/m3. The tank is connected to a high-pressure
supply line through a valve. The valve is opened, and
air is allowed to enter the tank until the density in the
tank rises to 7.20 kg/m3. Determine the mass of air that
has entered the tank.
3. The turbomachines conveying air are classified
usually as fans (p2/p1 < 1.3), blowers (1.3 < p2/p1 < 3)
and compressors (3 < p2/p1). Assuming p1 = 1 bar inlet
pressure, t1 = 20°C inlet temperature and isentropic
process (k = 1.4), find the relative density change (𝜌2𝜌1)/𝜌1 at the fan-blower border and the t2 outlet
temperature at the blower - compressor border.
(Solution: (𝜌2 - 𝜌1)/𝜌1= 20.6%, t2 = 128.1° C)
5.
6. Water flows through a horizontal pipe at a rate of 1
gal/s. The pipe consists of two sections of diameters 4
in and 2 in with a smooth reducing section. The pressure
difference between the two pipe sections is measured
by a mercury manometer. Neglecting frictional effects,
determine the differential height of mercury between
the two pipe sections. (Solution: 0.52 in)
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