Proceedings of the KSME Conference (대한기계학회:학술대회논문집)
- 2008.11b
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- Pages.2548-2553
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- 2008
Prediction of Hover Performance on Development of Small-Scale UAV using Numerical and Experimental Approach
실험을 통한 소형 무인헬리콥터의 공력인자 도출 및 제자리 비행 성능 예측
- Published : 2008.11.05
Abstract
Prediction of the rotor blade performance is important for determining design factors such as weight and size in development of a small-scale helicopter. Generally, prediction of helicopter performance means the estimation of the power required for a given flight condition. However, due to lack of test data and analyzed results for small-scale rotor blade operated at low Reynolds numbers (
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