机构地区: 西北工业大学
出 处: 《强度与环境》 1995年第4期37-40,共4页
摘 要: 针对某型飞机平尾额振速度偏低的实际问题,详细探讨了利用配重提高颤振速度的方案。分析方法及所得结果将有助于改善平尾的顾振特性,从而提高额振速度。 It is a very important actual problem to be solved in aircraft engineering that the flutter speed of horizontal tail is lower than designed. To this end, by making use of attached weights, several measures are put forward to improve the flutter properties of horizontal tail of certain type aircraft. The analytical methods and the results obtained will be conductive to increase the flutter speed of horizontal tail.
领 域: [航空宇航科学与技术] [航空宇航科学技术]