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Handbook of Turbomachinery Second Edition Revised - Ventech!

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addition, quantitative flow velocity measurements can be made simultaneously<br />

if the visualization technique allows for the motion <strong>of</strong> discrete<br />

particles to be viewed by high-speed optical devices. This study is performed<br />

usually inside an up-scaled transparent model. One <strong>of</strong> the rather simple<br />

visualization techniques can be based on application <strong>of</strong> neutrally buoyant<br />

helium-filled soap bubbles <strong>of</strong> controlled size that are produced by a separate<br />

bubble generator. The bubbles trace air-flow patterns at speeds as high as<br />

200 fps. Since they follow the flow streamlines, the bubbles rarely collide<br />

with objects in the airstream and are extremely durable. The motion <strong>of</strong> the<br />

bubbles at lower speeds, up to 30 fps, can be photographed using<br />

conventional film and lighting. For higher speeds, special film and lighting<br />

are required. With an interrupted light source, the motion appears as broken<br />

streaks on the photograph, which can be used to obtain a quantitative<br />

measurement <strong>of</strong> local velocities. The primary objective <strong>of</strong> these experiments<br />

is to quickly identify any stagnant zones, recirculation, and separation, or<br />

any anomalies in the flow behavior that could compromise the projected<br />

cooling performance. If any <strong>of</strong> these flow phenomena exist, it may be<br />

necessary to incorporate design changes to overcome them.<br />

A highly recommenced experimental technique, which is known as<br />

thermal imaging, was introduced by Hippensteele et al. [126] and since then<br />

has been used extensively for direct local convective heat-transfer measurements<br />

within cooling passages. Improvements in video systems brought<br />

tremendous enhancement <strong>of</strong> the imaging method. The Thermochromic<br />

Liquid Crystal (TLC) coating may be described as an organic compound<br />

existing in the state between its solid and liquid phases. When its molecules<br />

are in a disturbed state (caused, for example, by increased temperature or<br />

mechanical shear), their axes are rotated, leading to bright reflected colors <strong>of</strong><br />

light. The visible effect is shown through a change from colorless to red. As<br />

the temperature is raised further, the colors pass through a range <strong>of</strong> the<br />

visible spectrum to blue/violet and finally to colorless again at higher<br />

temperatures. A primary advantage <strong>of</strong> the liquid-crystal coating is its<br />

reversible state, which allows a number <strong>of</strong> experiments to be performed<br />

without reapplying the coating and also provides redundant data during the<br />

same test if transitions <strong>of</strong> more than one color are recorded. Data reduced<br />

from thermal imaging can be presented in a pseudo-color plot <strong>of</strong> very finesize<br />

pixels, representing the heat-transfer matrix <strong>of</strong> the entire airfoil internal<br />

passage or one particular area. Each color corresponds to a particular range<br />

<strong>of</strong> heat-transfer coefficients. These values define internal heat-transfer<br />

boundary conditions required for thermal analysis.<br />

The liquid crystal (for example, Hallcrest, R35C1W) is sprayed evenly<br />

on the inner surface <strong>of</strong> the transparent model before testing. For an<br />

optimum visual background for the liquid crystal display, the test surface is<br />

Copyright © 2003 Marcel Dekker, Inc.

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