论文部分内容阅读
本文介绍飞机结冰的机理和条件、分析平尾前缘生成双角冰的危害。通过理论分析和风洞试验,对某机平尾前缘结角冰的气动特性和飞行特性作了初步的研究和预测。提出了平尾结冰时安全着陆的技术措施。
This article introduces the mechanism and conditions of aircraft icing and analyzes the hazards of generating ice horn at the leading edge of the tail. Through theoretical analysis and wind tunnel test, the aerodynamic characteristics and flight characteristics of the leading ice of a tail end of a certain plane are preliminarily researched and predicted. The technical measures of landing safely in flat-tail freezing are put forward.