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slavikrds [6]
3 years ago
14

Find the minimum diameter of an alloy, tensile strength 75 MPa, needed to support a 30 kN load.

Engineering
1 answer:
Naya [18.7K]3 years ago
7 0

Answer:

The minimum diameter to withstand such tensile strength is 22.568 mm.

Explanation:

The allow is experimenting an axial load, so that stress formula for cylidrical sample is:

\sigma = \frac{P}{A_{c}}

\sigma = \frac{4\cdot P}{\pi \cdot D^{2}}

Where:

\sigma - Normal stress, measured in kilopascals.

P - Axial load, measured in kilonewtons.

A_{c} - Cross section area, measured in square meters.

D - Diameter, measured in meters.

Given that \sigma = 75\times 10^{3}\,kPa and P = 30\,kN, diameter is now cleared and computed at last:

D^{2} = \frac{4\cdot P}{\pi \cdot \sigma}

D = 2\sqrt{\frac{P}{\pi \cdot \sigma} }

D = 2 \sqrt{\frac{30\,kN}{\pi \cdot (75\times 10^{3}\,kPa)} }

D = 0.0225\,m

D = 22.568\,mm

The minimum diameter to withstand such tensile strength is 22.568 mm.

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8 0
3 years ago
It is given that 50 kg/sec of air at 288.2k is iesntropically compressed from 1 to 12 atm. Assuming a calorically perfect gas, d
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Data;

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  • T = 288.2K
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<h3>Exit Temperature </h3>

The exit temperature of the gas can be calculated isentropically as

\frac{T_2}{T_1} = (\frac{P_2}{P_1})^\frac{y-1}{y}\\ y = 1.4\\ C_p= 1.005 Kj/kg.K\\

Let's substitute the values into the formula

\frac{T_2}{T_1} = (\frac{P_2}{P_1})^\frac{y-1}{y} \\\frac{T_2}{288.2} = (\frac{12}{1})^\frac{1.4-1}{1.4} \\ T_2 = 586.18K

The exit temperature is 586.18K

<h3>The Compressor input power</h3>

The compressor input power is calculated as

P= mC_p(T_2-T_1)\\P = 50*1.005*(586.18-288.2)\\P= 14973.53kW

The compressor input power is 14973.53kW

Learn more on exit temperature and compressor input power here;

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Tha's just another symbol for a switch, but this one specifies that the switch is a push-button type of switch.

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