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alekssr [168]
3 years ago
12

A desktop computer is to be cooled by a fan whose flow rate is 0.34 m3/min. Determine the mass flow rate of air through the fan

at an elevation of 3400 m where the air density is 0.7 kg/m3. Also, if the average velocity of air is not to exceed 103 m/min, determine the diameter of the casing of the fan.
Engineering
1 answer:
erik [133]3 years ago
3 0

Answer:65 mm

Explanation:

Given

Flow rate \dot{V}=0.34\ m^3/min

density of air \rho =0.7\ kg/m^3

average velocity of air v_{avg}=103\ m/min

Mass flow rate is given by

\dot{m}=\rho \times \dot{V}

\dot{m}=0.7\times 0.34

\dot{m}=0.238\ kg/min

And Flow rate can be written as

\dot{V}=A\cdot v_{avg}

Where A =Area of cross-section

0.34=\frac{\pi}{4}d^2\cdot v_{avg}

0.34=\frac{\pi}{4}\times d^2\times 103

d=0.0648\ m

d=64.8\approx 65\ mm

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The Reynolds number is the major parameter that relates fluid flow momentum to friction forces. How is the Reynolds number defin
fiasKO [112]

Answer:

Reynolds number determines whether a flow is laminar or turbulent flow.

Explanation:

Reynolds number is defined as ratio of inertia force to the viscous force. it is a dimension less  number. Reynolds number is used to describe the type of flow in a fluid whether it is laminar flow or turbulent flow. Reynolds number is denoted by Re.

When Reynolds number is in the range of 0 to 2000, the flow is considered to be laminar.

When Reynolds number is in the range of 2000 to 4000, the flow is considered to be transition.

And when Reynolds number is more than 4000, the flow is turbulent flow.

                     The boundary layer thickness for a fluid is given by

                                      δ = \frac{5\times x}{\sqrt{Re}}

where δ is boundary layer thickness

           x is distance from the leading edge

           Re is Reynolds number

Thus from the above boundary layer thickness equation, we can see that the boundary layer thickness varies inversely to square root of reynolds number.

8 0
3 years ago
What invention would you argue most impacted mechanical engineering
Law Incorporation [45]

Answer:

The wheel

Explanation:

3 0
3 years ago
Sea B = 5.00 m a 60.0°. Sea C que tiene la misma magnitud que A y un ángulo de dirección mayor que el de A en 25.0°. Sea A ⦁ B =
uranmaximum [27]

Answer:

\| \vec A \| = 6.163\,m

Explanation:

Sean A, B y C vectores coplanares tal que:

\vec A = (\| \vec A \|\cdot \cos \theta_{A},\| \vec A \|\cdot \sin \theta_{A}), \vec B = (\| \vec B \|\cdot \cos \theta_{B},\| \vec B \|\cdot \sin \theta_{B}) y \vec C = (\| \vec C \|\cdot \cos \theta_{C},\| \vec C \|\cdot \sin \theta_{C})

Donde \| \vec A \|, \| \vec B \| y \| \vec C \| son las normas o magnitudes respectivas de los vectores A, B y C, mientras que \theta_{A}, \theta_{B} y \theta_{C} son las direcciones respectivas de aquellos vectores, medidas en grados sexagesimales.

Por definición de producto escalar, se encuentra que:

\vec A \,\bullet\, \vec B = \|\vec A \| \| \vec B \| \cos \theta_{B}\cdot \cos \theta_{A} + \|\vec A \| \| \vec B \| \sin \theta_{B}\cdot \sin \theta_{A}

\vec B \,\bullet\, \vec C = \|\vec B \| \| \vec C \| \cos \theta_{B}\cdot \cos \theta_{C} + \|\vec B \| \| \vec C \| \sin \theta_{B}\cdot \sin \theta_{C}

Asimismo, se sabe que \| \vec B \| = 5\,m, \theta_{B} = 60^{\circ}, \vec A \,\bullet \,\vec B = 30\,m^{2}, \vec B\, \bullet\, \vec C = 35\,m^{2}, \|\vec A \| = \| \vec C \| y \theta_{C} = \theta_{A} + 25^{\circ}. Entonces, las ecuaciones quedan simplificadas como siguen:

30\,m^{2} = 5\|\vec A \| \cdot (\cos 60^{\circ}\cdot \cos \theta_{A} + \sin 60^{\circ}\cdot \sin \theta_{A})

35\,m^{2} = 5\|\vec A \| \cdot [\cos 60^{\circ}\cdot \cos (\theta_{A}+25^{\circ}) + \sin 60^{\circ}\cdot \sin (\theta_{A}+25^{\circ})]

Es decir,

30\,m^{2} = \| \vec A \| \cdot (2.5\cdot \cos \theta_{A} + 4.330\cdot \sin \theta_{A})

35\,m^{2} = \| \vec A \| \cdot [2.5\cdot \cos (\theta_{A}+25^{\circ})+4.330\cdot \sin (\theta_{A}+25^{\circ}})]

Luego, se aplica las siguientes identidades trigonométricas para sumas de ángulos:

\cos (\theta_{A}+25^{\circ}) = \cos \theta_{A}\cdot \cos 25^{\circ} - \sin \theta_{A}\cdot \sin 25^{\circ}

\sin (\theta_{A}+25^{\circ}) = \sin \theta_{A}\cdot \cos 25^{\circ} + \cos \theta_{A} \cdot \sin 25^{\circ}

Es decir,

\cos (\theta_{A}+25^{\circ}) = 0.906\cdot \cos \theta_{A} - 0.423 \cdot \sin \theta_{A}

\sin (\theta_{A}+25^{\circ}) = 0.906\cdot \sin \theta_{A} + 0.423 \cdot \cos \theta_{A}

Las nuevas expresiones son las siguientes:

30\,m^{2} = \| \vec A \| \cdot (2.5\cdot \cos \theta_{A} + 4.330\cdot \sin \theta_{A})

35\,m^{2} = \| \vec A \| \cdot [2.5\cdot (0.906\cdot \cos \theta_{A} - 0.423 \cdot \sin \theta_{A})+4.330\cdot (0.906\cdot \sin \theta_{A} + 0.423 \cdot \cos \theta_{A})]

Ahora se simplifican las expresiones, se elimina la norma de \vec A y se desarrolla y simplifica la ecuación resultante:

30\,m^{2} = \| \vec A \| \cdot (2.5\cdot \cos \theta_{A} + 4.330\cdot \sin \theta_{A})

35\,m^{2} = \| \vec A \| \cdot (4.097\cdot \cos \theta_{A} +2.865\cdot \sin \theta_{A})

\frac{30\,m^{2}}{2.5\cdot \cos \theta_{A}+ 4.330\cdot \sin \theta_{A}} = \frac{35\,m^{2}}{4.097\cdot \cos \theta_{A} + 2.865\cdot \sin \theta_{A}}

30\cdot (4.097\cdot \cos \theta_{A} + 2.865\cdot \sin \theta_{A}) = 35\cdot (2.5\cdot \cos \theta_{A}+4.330\cdot \sin \theta_{A})

122.91\cdot \cos \theta_{A} + 85.95\cdot \sin \theta_{A} = 87.5\cdot \cos \theta_{A} + 151.55\cdot \sin \theta_{A}

35.41\cdot \cos \theta_{A} = 65.6\cdot \sin \theta_{A}

\tan \theta_{A} = \frac{35.41}{65.6}

\tan \theta_{A} = 0.540

Ahora se determina el ángulo de \vec A:

\theta_{A} = \tan^{-1} \left(0.540\right)

La función tangente es positiva en el primer y tercer cuadrantes y tiene un periodicidad de 180 grados, entonces existen al menos dos soluciones del ángulo citado:

\theta_{A, 1} \approx 28.369^{\circ} y \theta_{A, 2} \approx 208.369^{\circ}

Ahora, la magnitud de \vec A es:

\| \vec A \| = \frac{35\,m^{2}}{4.097\cdot \cos 28.369^{\circ} + 2.865\cdot \sin 28.369^{\circ}}

\| \vec A \| = 6.163\,m

8 0
4 years ago
Air is to be compressed so that its volume is reduced to half of its original volume if the initial pressure is 200 kPa and the
Alex_Xolod [135]

Answer:

P_{2} = 527.803\,kPa

Explanation:

The politropic relationship for a isentropic process is:

\frac{P_{2}}{P_{1}} = \left(\frac{V_{1}}{V_{2}}  \right)^{\gamma}

Where \gamma is the ratio of specific heats

The final pressure is:

P_{2} = P_{1}\cdot \left(\frac{V_{1}}{V_{2}}\right)^{\gamma}

P_{2} = (200\,kPa)\cdot (2)^{1.4}

P_{2} = 527.803\,kPa

7 0
3 years ago
Hey answr this sajida Yusof
Allisa [31]
What do u need? Rusbaisuwvwbs
5 0
3 years ago
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