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混合翼型对扑翼推进性能影响分析
Alternative TitlePropulsive performance of complex flapping foils
曹永辉; 朝黎明; 丁浩; 赵红印
Department机器人学研究室
Source Publication上海交通大学学报
ISSN1006-2467
2016
Volume50Issue:8Pages:1228-1232, 1240
Indexed ByEI ; CSCD
EI Accession number20163802821728
CSCD IDCSCD:5791665
Contribution Rank3
Funding Organization西北工业大学研究生创意创新种子基金(Z2015054)资助
Keyword扑翼 混合翼型 推进性能
Abstract以NACA0006翼型为基准翼型,将其前缘部分更换为相对最大厚度较大的NACA0008、NACA0010、NACA0015和NACA0020翼型前缘部分,组成混合翼型。通过流体仿真软件Fluent14.5对基准翼型及混合翼型进行数值模拟计算,并分析扑翼运动的推进性能。结果表明:混合翼型相较于基准翼型对扑翼运动推力系数和推进效率有显著提高。
Other AbstractThe NACA0006 foil was used as the baseline, the leading edge of complex flapping foils was replaced as the counterpart of thicker NACA foil (NACA0008, NACA0010, NACA0015 and NACA0020). Fluent 14.5 was used in numerical studies, considering the propulsive performance of all complex flapping foils. The conclusion indicates that complex flapping foils have a more propulsive performance.
Language中文
Citation statistics
Cited Times:1[CSCD]   [CSCD Record]
Document Type期刊论文
Identifierhttp://ir.sia.cn/handle/173321/19228
Collection机器人学研究室
Corresponding Author曹永辉
Affiliation1.西北工业大学航海学院
2.中国船舶重工集团公司第七一三研究所
3.中国科学院沈阳自动化研究所
Recommended Citation
GB/T 7714
曹永辉,朝黎明,丁浩,等. 混合翼型对扑翼推进性能影响分析[J]. 上海交通大学学报,2016,50(8):1228-1232, 1240.
APA 曹永辉,朝黎明,丁浩,&赵红印.(2016).混合翼型对扑翼推进性能影响分析.上海交通大学学报,50(8),1228-1232, 1240.
MLA 曹永辉,et al."混合翼型对扑翼推进性能影响分析".上海交通大学学报 50.8(2016):1228-1232, 1240.
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