摘要
为了满足型号设计的需要,掌握战术导弹折叠尾翼在发射初始时的展开特性,对两种折叠翼快速展开的测试技术进行了试验研究。详细说明了两种测试方法的原理、测试量之间的比较、测试结果的分析。两种方案均在北京空气动力研究所(BIA)的一座低速风洞中进行了多次重复试验比较,测试结果表明两种方法均成熟可靠,可以用于战术导弹的实际设计中。
For satisfying the demands of missile design and mastering the deploying characteristics of folding wings at the beginning of launch, the paper introduces the differences between two deploying methods and results. The principles of two methods are illustrated in detail. Both plans have been tested for many times in a low speed wind tunnel of Beijing Institute of Aerodynamics (BIA). The results indicate that the tests are successful and reliable which can be used in design.
出处
《流体力学实验与测量》
CSCD
北大核心
2003年第2期70-73,共4页
Experiments and Measurements in Fluid Mechanics
关键词
战术导弹
折叠翼
展开方法
测试
低速风洞
folding wings
measurement technology
deploying method
wind tunnel test
