...
首页> 外文期刊>Acta astronautica >Insulator ablation modes in different impact conditions of alumina droplets onto wall surfaces
【24h】

Insulator ablation modes in different impact conditions of alumina droplets onto wall surfaces

机译:氧化铝液滴在壁面上不同冲击条件下的绝缘子烧蚀模式

获取原文
获取原文并翻译 | 示例
   

获取外文期刊封面封底 >>

       

摘要

Current understanding of insulator ablation modes under different alumina droplet impact conditions onto wall surfaces in solid rocket motors (SRM) is limited. This study uses theoretical analysis and numerical calculations to design a lab-scale experimental device and an ultra-high-temperature heat flow gauge. Alumina droplet/insulator wall surface impact characteristics such as erosion angle, speed, and droplets size distribution are discussed based on the resulting experimental data using the proposed design. Three ablation modes are established according to the droplet speed threshold: the weak erosion state, deposition state, and strong erosion state. On this basis, heat transfer characteristics are studied under the condition of high-density, two-phase flow and the general rules of the wall heat increment with droplet concentration, size, and velocity under different droplet/wall impact modes are obtained. Finally, discussing multi-factor variables, the coupling relationship among the thermal increment, thermal chemical ablation, and mechanical erosion under droplet/wall surface action is analysed, providing insights toward establishing an insulator ablation model.
机译:目前对固体火箭发动机(SRM)中不同氧化铝液滴撞击条件对壁表面的绝缘子烧蚀模式的了解有限。本研究使用理论分析和数值计算来设计实验室规模的实验设备和超高温热流计。使用所提出的设计,基于所得的实验数据,讨论了氧化铝液滴/绝缘体壁表面的冲击特性,例如腐蚀角度,速度和液滴尺寸分布。根据液滴速度阈值建立了三种烧蚀模式:弱腐蚀状态,沉积状态和强腐蚀状态。在此基础上,研究了高密度,两相流条件下的传热特性,得到了不同液滴/壁撞击方式下壁热量随液滴浓度,大小和速度的增加的一般规律。最后,讨论了多因素变量,分析了液滴/壁表面作用下热增量,热化学烧蚀和机械腐蚀之间的耦合关系,为建立绝缘体烧蚀模型提供了见识。

著录项

相似文献

  • 外文文献
  • 中文文献
  • 专利
获取原文

客服邮箱:kefu@zhangqiaokeyan.com

京公网安备:11010802029741号 ICP备案号:京ICP备15016152号-6 六维联合信息科技 (北京) 有限公司©版权所有
  • 客服微信

  • 服务号