ISA 1932 Conical nozzle shape diffuser Throat tap 1es 15° 0.7d 2 Flow (c)

Q: For cases shown in fig.Q2. Describe and discuss the fluid flow properties for each case separately.…

A: Flow of fluid:The fluid flows from one point to another by pressure difference. The fluid flows from…

Q: I nree pipes steadiy aenver water at 20°C to a large exit pipe in Fig. P3.8. The velocity V, = 5…

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Q: An airplane uses a pitot-static tube as a velocimeter. Themeasurements, with their uncertainties,…

A: Given data: Static temperature, T = - 110C = 262 K Static pressure, P = 60 kPa Pressure difference ,…

Q: JI Air stream flow in a convergent - divergent nozzle, with a stagnation pressure of 120 kPa, the…

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Q: Air flows at high speed through a Herschel venturi monitoredby a mercury manometer, as shown in Fig.…

A: Given data, Determine the density of fluid by using the ideal gas equation,

Q: 26 (a) Explain briefly the difference between incompressible and compressible fluid flow.

A: Compressible and incompressible flow will be defined based upon density of fluid due to application…

Q: Water (density 1000 kg/m) flows through an inclined pipe of uniform diameter. The velocity. pressure…

A: Bernoulli's equation states that if a fluid is ideal, incompressible and steady, then the total…

Q: A gas, assumed ideal, flows isentropically from point 1,where the velocity is negligible, the…

A: Hello. Since your question has multiple sub-parts, we will solve first three sub-parts for you. If…

Q: An ideal gas flows adiabatically through a duct. At section1, p1 =140 kPa, T1 = 2608C, and V1 = 75…

A: Since multiple questions are asked and also it is not specified which question to solve, so as per…

Q: A, = 0.001184 m², A2 = 0.001065 m², p2 = 142 kPa, T2 = 133 °C, v2 = 294 m-s", find (a) Remaining…

A: Given data: Cross-sectional area at section 1, A1=0.001184 m2 Cross-sectional area at section 2,…

Q: diverging nozzle. The air has tota Scm, M=0.8 and V =300 m/s. det (for air tal

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Q: Air, at stagnation conditions of 500 K and 200 kPa, flows through a nozzle. At section 1, where the…

A: The Answer is Below

Q: wind tunnel nozzie consists of a smooth contraction from Az = 0.2 m². The outlet velocity is Uz =40…

A: Draw the diagram- Given -A1=0.6m2A2=0.2 m2V2=40 m/sP2=101.6 kPaP=1.225 kg/m3(constant due to in…

Q: In a compressible isentropic flow a fluid inters into a throat other than sonic velocity. Discuss…

A: The figure below represents the flow of fluid through the different sections. Point (1) represents…

Q: /2 Air flows from a reservoir where Pa and T-500 K through a throat to section 1 P =300 Figure where…

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Q: Pump Pam = 100 kPa D= 3 cm The pump in Fig. P3.146 draws gasoline at 20°C from a reservoir. Pumps…

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Q: 1. Air, with stagnation conditions of 800 kPa and 100 °C, ex pands isentropically to a section of a…

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Q: The insulated tank in Fig. P3.182 is to be fi lled from a highpressureair supply. Initial conditions…

A: The initial mass inside the system can be calculated as,

Q: Carbon dioxide convergent-divergent to a Lule of 60 m / s, 310 °C and 300 kPa in its case, it enters…

A: Nozzle: Nozzle is a device which having varying in cross section, in which pressure is reduced by…

Q: Q: Helium, in a large tank at 100 °C and 400 kPa, discharges to a receiver through a…

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Q: How do the compressible pipe flow formulas behave forsmall pressure drops? Let air at 20°C enter a…

A: Given: The temperature of the air at the entry of the tube is T1 = 20 oC. The friction coefficient…

Q: Q5. A duct of a friction length of fx/D = 124 is connected to a Duct reservoir. A nozzle is attached…

A: Given: Receiver pressure, Pe=103.4 kPafLD=12.4Nozzle exit area, Ae=6 cm2Nozzle inlet area, A3=9…

Q: Air fl ows adiabatically in a 3-cm-diameter duct, withf 5 0.018. At the entrance, T1 = 323 K, p1…

A: Given data:  Air flows adiabatically Duct diameter (D) = 3 cm = 0.003 m Friction factor (f)  = 0.018…

Q: What is the atmospheric pressure? kPa Required informetion Ar in a tank at 120 kPa and 300 K…

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Q: The centrifugal pump of Fig.  develops a fl owrate of 4200 gal/min of gasoline at 20°C with…

A: Given: Speed of the blade = 1750 rpm flow rate,  Q=4200 gal/min=4200×0.133681×160=9.357 ft3/s…

Q: Q1// Air stream flow in a convergent- divergent nozzle, with a stagnation pressure of 120 kPa, the…

A: The nozzle is both convergent and divergent. The forward section of the nozzle is convergent,…

Q: A2 = 0.018 m?, v, = 54 m-s', p, = 76 kPa

A: Given                   Diverging area, A = 0.018 m2 Pressure at diverging duct, P = 76 kPa Find…

Q: 3. What is the volume (h x A) of this reservoir (m) if h is the height of reservoir (m) and its…

A: This problem is related to fluid mechanics. Fluid mechanics is the subject of mechanical engineering…

Q: Q3:/ A large reservoir at (600 k) supplies air flow through a converging-diverging duct with throat…

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Q: A large room uses a fan to draw in atmospheric air at 20°Cthrough a 30-cm by 30-cm commercial-steel…

A: (a) The density of the air is: ρair=1.2kgm3 For commercial steel, ε=0.046 mm Side length, DH=30 cm…

Q: If there are no shock waves and the pressure at one ductsection in Fig.  is 55.5 kPa, what is the…

A: given data as per the question The temperature of tank =400 k The pressure of tank =300 Kpa…

Q: A pipe connecting two reservoirs, as in Fig., containsa thin-plate orifice. For water flow at 20°C,…

A: Given data: The temperature of water is T= 20 oC. The length of the pipe is L = 100 m. The diameter…

Q: An experimental scramjet aircraft is flying at an altitude of 25,000m at Mach 5. Considering it;s…

A: Given: M1 =5  delta = 5 deg P2/P1 = ?

Q: D, -6 cm Three pipes steadily deliver water at 20°C to a large exit pipe in Fig. P3.8. The D;=5 cm…

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Q: Q5: Steady, one-dim., comp. flow, A, = 0.016 m?, v1 = 120 m-s1, P1=2.65 kg-m, p1 = 170 kPa A2 =…

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Q: ven A)A horizontal gas well of 2000 ft long is draining an area of approximately 120 acres. The…

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