前缘角冰几何参数对翼型失速特性的影响

Q3 Engineering
Binbin Zhao, Xianping Li, Jie Li, Heng Zhang
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引用次数: 0

摘要

喇叭型冰的不规则特征和几何随机性显著,分离行为复杂。导致失速性能发生本质变化的机制和因素尚不清楚。根据大型客机适航审定的实际要求,基于典型的超临界翼型和结冰环境,构造了一组不同参数的喇叭型冰型。结合风洞试验和数值模拟方法,系统分析了翼型失速特性对冰高和冰角变化的参数敏感性,总结了失速过程中冰形参数导致分离气泡发展变化的本质影响机制,为大型客机冰上适航审定提供了理论依据。
本文章由计算机程序翻译,如有差异,请以英文原文为准。
Influence of geometric parameters of leading edge horn-ice on stall characteristics of airfoil
The irregular characteristics and geometric randomness of horn-type ice are significant while the behaviors of separation are complex. The mechanism and factor leading to the essential change of stall performance are still not clear. According to actual requirements of airworthiness certification of a large passenger aircraft, a family of horn-type ice shapes with different parameters are constructed based on typical supercritical airfoil and icing environment. By combining with wind tunnel test and numerical simulation methods, the parameter sensitivity of airfoil stall characteristics to the change of ice height and angle is systematically analyzed and the essential influence mechanism of the ice shape parameters leading to the change of separation bubble development under stall process is summarized, which provides a theoretical basis for ice airworthiness certification of large passenger aircraft.
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来源期刊
西北工业大学学报
西北工业大学学报 Engineering-Engineering (all)
CiteScore
1.30
自引率
0.00%
发文量
6201
审稿时长
12 weeks
期刊介绍:
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