【24h】

Instantaneous RRMI of Iron Rods in Reduced Gravity

机译:降低重力的铁棒的瞬时RRMI

获取原文
获取原文并翻译 | 示例

摘要

Standard upward-burning promoted ignition tests ("Standard Test Method for Determining the Combustion Behavior of Metallic Materials in Oxygen-Enriched Atmospheres," ASTM G4-124or "Flammability, Odor, Offgassing, and Compatibility Requirements and Test Procedures for Materials in Environments that Support Combustion," NASA-STD-6001, NASA Test 14) were performed on cylindrical iron (99.95% pure) rods in various oxygen purities (95.0-99.98%) in reduced gravity onboard NASA JSC's KC-135 to investigate the effect of gravity on the regression rate of the melting interface. Visual analysis of experiments agrees with previous published observations showing distinct motions of the molten mass attached to the solid rod during testing. Using an ultrasonic technique to record the real-time rod length, comparison of the instantaneous regression rate of the melting interface and visual recording shows a non-steady-state regression rate of the melting interface for the duration of a test. Precessional motion is associated with a higher regression rate of the melting interface than for test periods in which the molten mass does not show lateral motion. The transition between the two types of molten mass motion during a test was accompanied by a reduced regression rate of the melting interface, approximately 15-50% of the average regression rate of the melting interface for the entire test.
机译:标准的向上燃烧促进点火测试(“确定富氧气氛中金属材料燃烧行为的标准测试方法”,ASTM G4-124或“支持环境的材料的易燃性,气味,除气和相容性要求及测试程序在NASA JSC的KC-135上以降低的重力对各种氧气纯度(95.0-99.98%)的圆柱铁棒(纯度99.95%)进行燃烧,“ NASA-STD-6001,NASA测试14”,以研究重力对熔化界面的回归率。实验的视觉分析与先前发表的观察结果一致,该观察结果显示了在测试过程中附着在固体棒上的熔融物料的明显运动。使用超声波技术记录实时棒长,熔融界面的瞬时回归速率与可视记录的比较显示了在测试期间熔融界面的非稳态回归速率。与在熔融物质不显示横向运动的测试期间相比,进动运动与熔融界面的更高的回归速率相关。在测试过程中,两种类型的熔融体运动之间的过渡伴随着熔融界面的降低,这是整个测试过程中熔融界面的平均降低率的大约15-50%。

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