首页> 外文会议>International space conference of Pacific-basin societies >Investigation on Slot Air Film Cooling of Ramjet Combustion Chamber
【24h】

Investigation on Slot Air Film Cooling of Ramjet Combustion Chamber

机译:拉米特燃烧室槽空气薄膜冷却研究

获取原文

摘要

In this paper,two methods were used to analysing and calculating the fields of slot air film cooling. One method was the engineering simulation based on experimental formulas, and the other was numerical simulation. The main factors influencing on the film cooling efficiency was investigated detailedly, especially the flow rate of the air injection from the cooling slot. A prediction of the slot film cooling efficiency was done according to the ramjet combustion chamber characterized by higher Mach number and longer duration of flight. The slot film cooling structure scheme in the combustion chamber with higher temperature was given as a reference.
机译:本文使用了两种方法来分析和计算槽空气膜冷却场的田地。一种方法是基于实验公式的工程模拟,另一个方法是数值模拟。细节研究了影响薄膜冷却效率的主要因素,特别是从冷却槽的空气喷射的流速。根据Ramjet燃烧室的特征在于以更高的马赫数和较长的飞行持续时间来完成对槽膜冷却效率的预测。将燃烧室中的槽膜冷却结构方案作为参考作为参考。

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