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Aerodynamics and Design for Ultra-Low Reynolds Number Flight

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Chapter 5<br />

The test fixtures <strong>for</strong> measuring thrust consist of an aluminum bar with a motor-mount on<br />

one end <strong>and</strong> a contact point <strong>for</strong> an electronic two milligram-accurate balance on the<br />

other. It is supported at near mid-span by a shaft <strong>and</strong> ball-bearings, providing a single<br />

axis of rotation. Upward thrust is transferred to a downward <strong>for</strong>ce on the balance that<br />

can be read directly, then converted to the thrust value by the ratio of the moment arms.<br />

Two fixtures have been fabricated to cover a wider range of rotor sizes.<br />

The smaller set of test equipment, configured <strong>for</strong> thrust measurement, is pictured in<br />

Figure 5.5. Rotor torque <strong>for</strong> larger rotors may be measured by mounting the rotor <strong>and</strong><br />

motor to the shaft of the balance bar with the rotor axis of rotation parallel to the shaft.<br />

The registered <strong>for</strong>ce on the balance is converted to a torque across the moment arm from<br />

the balance contact point to the aluminum bar’s axis of rotation. This configuration is<br />

shown in Figure 5.6.<br />

80

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