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