本文为美国威奇塔州立大学（作者：Monal Pankaj Merchant）的硕士论文，共55页。

最近UAV和MAV的发展增加了对小型螺旋桨性能数据的强烈需求。螺旋桨性能对这些飞机的成功至关重要，保证性能需要准确的实验数据。这些螺旋桨在低雷诺数（30000到300000之间）下工作，使用较大螺旋桨的性能数据进行缩比是不准确的。威奇塔州立大学设计、开发、验证了一套完整的螺旋桨测试系统，能够准确可靠地测量小型螺旋桨的性能。我们已经绘制了大量螺旋桨的性能图表，并建立了性能数据库。本文讨论了这一测量系统的显著特点，以及图表中测量的30多个螺旋桨数据。

The recent increase in the development ofUAV’s and MAV’s has created a strong demand for small propeller performancedata. Propeller performance is critical to the success of these aircraft andguaranteed performance demands accurate experimental data. These propellersoperate at low Reynolds numbers (between 30,000 and 300,000), renderingperformance scaling from larger counterparts inaccurate. An IntegratedPropulsion Test System has been designed, developed and validated at WichitaState University to accurately and reliably measure performance of smallpropellers. Performance of a large number of propellers has been charted and adatabase of performance data has been created. This thesis discusses thesalient features of this measurement system and data for a few of the, over 30propellers, charted.

1. 引言

2. 实验装置

3. 实验过程

4. 结果与讨论

5. 结论

6. 研究建议

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