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在运载火箭改进优化或新型运载火箭设计过程中,会遇到各种复杂的流动与传热问题。按照真实产品和物理过程直接建立的数值计算模型过于复杂,不同尺度的结构、流动与传热、长时间的飞行过程相互耦合,出现计算时间太长(数年)、收敛困难、程序调试困难等问题。针对初始条件复杂、飞行过程复杂、边界条件复杂3类具体问题,总结了3种相应的模型简化方法,分别是工程经验法、极限参数法、低维近似法,为推进剂复杂流动与传热的数值模拟提供参考。 相似文献
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G A Soffen 《Advances in Space Research (includes Cospar's Information Bulletin, Space Research Today)》1986,6(11):57-60
The emergence of the first life on the earth is now established as an early event, and closely related to the evolving earth. Laboratory experiments examining possible chemical events have revealed a multitude of plausible pathways. Lack of knowledge of the primitive terrestrial conditions contemporary with the evolving prebolic organic chemistry limits reconstruction techniques. The primitive earth's aqueous history is essential to unraveling this problem. Based on our current knowledge of other planets of the solar system, we do not expect close analogues to the early earth. We still do not know if there was a second origin or if only earth has life. This may depend upon the question of the survival of information bearing chemical systems in a dynamic or chaotic environment and the chemical protection afforded within such a system. Water is the central molecule of controversy: the blessing and the curse of the chemist. New and novel chemical mechanisms and systems abound. 相似文献
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Soffen GA 《Acta Astronautica》1997,41(4-10):609-611
The development of an Astrobiology Program is an extension of current exobiology programs. Astrobiology is the scientific study of the origin, distribution, evolution, and future of life in the universe. It encompasses exobiology; formation of elements, stars, planets, and organic molecules; initiation of replicating organisms; biological evolution; gravitational biology; and human exploration. Current interest in life on Mars provides the scientific community with an example of scientific inquiry that has mass appeal. Technology is mature enough to search for life in the universe. 相似文献
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运载火箭在飞行过程中需要进行姿态调整以满足入轨要求,贮箱内推进剂在外界干扰力的作用下将发生晃动,由此引入了诸如气液接触面积、蒸发、冷凝过程及推进剂流动变化等不确定影响因素。实际飞行过程尤其是进入滑行段的初始推进剂晃动对贮箱内气枕压力及推进剂流动行为具有重要影响。在调研国内外运载火箭末级飞行过程中低温贮箱压力及推进剂流动特性的基础上,建立仿真模型,采用流体体积函数方法(VOF)分析滑行段推进剂流动特性变化对贮箱气枕压力的影响。 相似文献
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推力室中压力剧烈振荡区域的燃烧特性分析 总被引:1,自引:1,他引:1
在不施加任何扰动的情况下,对液氧/煤油双组元液体火箭发动机模型燃烧室进行三维非稳态数值模拟,获得了其中的压力自激振荡现象。基于定义的能够辨识定容和定压燃烧特征的第三邓克尔数分析了压力剧烈振荡区域的燃烧特性。结果表明,在压力剧烈振荡区域内,第三邓克尔数取值很大,即发生了准定容燃烧或介于定容和定压之间的燃烧过程。可见尽管液体火箭发动机燃烧室整体表现为定压燃烧特性,但在头部附近区域出现了局部具有非定压特性的燃烧过程,其产生的压力膨胀波来不及迅速传播而使当地的压力迅速升高,形成了定容弹效应,从而导致了燃烧不稳定性的发生。该压力峰的传播及其与室壁相互作用在燃烧室中产生声学不稳定性,与研究燃烧不稳定性的定容弹试验机理相同。 相似文献
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