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AE 401-- Procedure -- Lab: Nozzle Performance - Clarkson University

AE 401-- Procedure -- Lab: Nozzle Performance - Clarkson University

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<strong>AE</strong> <strong>401</strong> – Spring 2005<br />

1 2 3 4 5<br />

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2.0mm<br />

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10 O<br />

Thrust Force [ N ]<br />

4.5<br />

4<br />

3.5<br />

3<br />

2.5<br />

2<br />

1.5<br />

1<br />

0.5<br />

0<br />

Calibration Data<br />

y = 0.044185x - 0.033807<br />

-0.5<br />

0 10 20 30 40 50 60 70 80 90 100<br />

Micrometer Reading<br />

Figure 1: <strong>Nozzle</strong> Geometries<br />

Figure 3: Micrometer calibration curve.<br />

A rotameter is used to measure the mass flow<br />

rate, ṁ, through the nozzle. The scale on the rotameter<br />

is incremented in millimeters. The calibration<br />

curve is used to convert from millimeters to the<br />

mass flow rate. The calibration curve is shown in<br />

Figure 4. Make sure you apply the density correction<br />

factor k that can be obtained from Figure 5 or<br />

Equation 17.<br />

9<br />

8<br />

Calibration Data<br />

y = 0.8895 + 0.0292x + 2.34e-5x 2<br />

7<br />

Figure 2: Apparatus for <strong>Nozzle</strong> Tests<br />

Instrumentation<br />

The thrust force is measured using what is effectively<br />

a beam type load cell. The nozzle is threaded<br />

into the end of a long section of tubing. The thrust<br />

force produced as a result of mass being thrown<br />

from the nozzle, causes the beam to deflect downward.<br />

From our strengths of materials studies, we<br />

know that a cantilever beam with concentrated load<br />

can be described as:<br />

y = F l3<br />

3EI<br />

(16)<br />

The modulus of elasticity, E, the length of the<br />

beam, l, and the moment of inertia, I, are all<br />

constant which indicates that the deflection of the<br />

beam, y should vary linearly with the thrust force,<br />

F . Figure 3 demonstrates this and provides an<br />

equation relating the displacement to thrust force.<br />

Air Flow Rate / 10 - 3 kg ⋅ s - 1<br />

6<br />

5<br />

4<br />

3<br />

2<br />

1<br />

0<br />

0 20 40 60 80 100 120 140 160 180 200 220 240<br />

Scale [ mm ]<br />

Figure 4: Calibration curve for 35E rotameter with<br />

duralumin float. Note: Curve is correct for ρ =<br />

1.2kg · m −2 . Multiply mass flow rate by correction<br />

factor, k, from Figure 5.<br />

The rotameter calibration correction factor, k,<br />

can be extracted from Figure 5. To obtain a reasonable<br />

estimate of the correction factor from the plot,<br />

the atmospheric pressure, P a and ambient temperature,<br />

T , must be measured. The atmospheric pressure<br />

can be measured using the mercury barometer<br />

located on the wall near the safety goggle cabinet.<br />

4

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