首页> 外文会议>30th AIAA/ASME/SAE/ASEE Joint Propulsion Conference June 27-29, 1994/Indianapolis, IN >Effect of Swirling on Burning Rate for Solid Rocket Motor(SRM)
【24h】

Effect of Swirling on Burning Rate for Solid Rocket Motor(SRM)

机译:旋流对固体火箭发动机燃速的影响

获取原文

摘要

An experimental study of swirling solid rocket motor(SSRM) has been completed. The effect of swirling on burning rate for SRM is emphasized in this paper. The experimental equipment is introduced and a lot of experimentla data are obtained. Based on researches done, a theoretical model for the prediction of the effect of swirling on burning rate for SSRM has been put forward and successfully used to calculate internal ballistic performance for SSRM. The prediction results of the theoretical model are consistent with the measured results.
机译:完成了涡旋固体火箭发动机的实验研究。本文强调了涡流对SRM燃烧速率的影响。介绍了实验设备并获得了大量实验数据。在进行研究的基础上,提出了一种预测SSRM涡流对燃烧速率影响的理论模型,并成功地用于计算SSRM的内部弹道性能。理论模型的预测结果与实测结果吻合。

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