轴对称件超塑约束胀形过程FEM模拟

采用大变形刚粘塑性有限元 ( FEM)模拟了圆板轴对称超塑约束胀形的贴模过程。研究了胀形件几何尺寸 (胀形高宽比 HP/RD)、材料速率敏感指数 m、摩擦因子 Am 对胀形件贴模过程 ,以及贴模方式对厚度不均的影响     

镍基高温合金铸件的晶粒组织控制──添加剂的影响

选用ＩＮ７３８ＬＣ镍基高温合金,研究了向熔体中加入碳化物、氮化物、硼及金属间化合物对合金冷凝后的晶粒尺寸、枝晶组织和初生碳化物形态等凝固组织特征的影响。结果发现,加入金属间化合物并控制合金液的均匀化处理过程可显著细化晶粒,并且对合金的结晶特性及凝固组织无不良影响。     

Cosmic ray modulation in the 3-D heliosphere

The basic physical processes that lead to the long-term modulation of cosmic rays by the solar wind have been known for many years. However our knowledge of the structure of the heliosphere, which determines which processes are most important for the modulation, and of the variation of this structure with time and solar activity level is still incomplete. Study of the modulation provides a tool for probing the scale and structure of the heliosphere. While the Pioneer and Voyager spacecraft are surveying the radial structure and extent of the heliosphere at modest heliographic latitudes, theUlysses mission is the first to undertake a nearly complete scan of the latitudinal structure of the modulated cosmic ray intensity in the inner heliosphere (R<5.4 AU).Ulysses will reach latitudes of 80°S in September 1994 and 80°N in July 1995 during the approach to minimum activity in the 11 year solar cycle. We present a first report of measurements extending to latitudes of 52°S, which show surprisingly little latitudinal effect in the modulated intensities and suggest that at this time modulation in the inner heliosphere may be much more spherically symmetric than had generally been believed based upon models and previous observations.     

Ulysses out-of-ecliptic observations of “27-day” variations in high energy cosmic ray intensity

We report the discovery that for latitudes above 40°S, the observed recurring modulation of cosmic rays and anomalous nuclei occurs without the detection byUlysses of the solar wind velocity and magnetic field recurring enhancements that have, heretofore at lower latitudes, defined corotating interaction regions—i.e., the mechanism producing the recurring intensity variations >40°S appears to be located beyond the radial range ofUlysses.     

火箭发动机－超音速扩压器－蒸汽引射泵组合式高空模拟试验系统的性能研究

通过对火箭发动机－超音速扩压器－蒸汽引射泵组合式高模拟系统的理论分析和实验研究，提出了扩大ＧＳ－１高空模拟试车台试验能力的几项新方案。     

微型固体火箭发动机用短点火延迟点火器研究

短的点火延迟期对某些微型固体火箭发动机尤为重要。文中引用固相点火理论，在诸多向推进剂表面供热的方式中，着重分析了起重要作用的对流换热，认为提高点火燃气的流速能明显地提高点火燃气对推进剂表面的热交换率，使推进剂表面很快达到发火温度，在微型固体火箭发动机的短点火延迟点火器设计中应用了这一理论，并获得了理想的效果。     

固体火箭燃烧室内微粒分布的实验研究

介绍一种实时脉冲取样器用于测定固体火箭燃烧室内凝相微粒尺寸分布技术，实验结果表明，含铝推进剂微粒呈二模态或三模分布，燃烧室内压力大，微粒趋大，燃烧室压力很小，微粒亦趋大，有一最小尺寸的压力值，残渣影响微粒尺寸测量，而推进剂燃烧特性将直接影响着微粒尺寸分布。     

超音速燃烧二元流场的数值模拟

由二元超音速燃烧流场垂直喷射Ｈ２的数值模拟计算，描述了缝隙喷嘴附近氧气与空气的混合和燃烧过程，使用两步化学反应，ＭａｃＣｏｒｍａｒｋ显式时间分裂法和Ｂａｌｄｗｉｎ－Ｌｏｍａｘ修正的代数湍流模型，计算超音速燃烧流场，得出了流线，静压，静温，Ｈ２和Ｈ２Ｏ浓度等值线图，反映了缝隙喷嘴附近回流区的大小，自动着火点的位置及火焰向主流的传播现象。     

两种新型含铜催化剂对RDX／AP催化热分解的研究

通过热分解试验，系统地研究了两种新型含铜催化剂对ＲＤＸ，ＡＰ，ＲＤＸ／ＡＰ的催化作用，由热分析图谱及动力学计算结果可以看出：ＹＢ对ＡＰ，ＱＣ对ＲＤＸ及ＹＢ＋ＱＣ对ＲＤＸ／ＡＰ的热分解有明显的催化作用，其推进剂的燃速测定结果也进一步证明其催化效果。     

固体发动机推力随机调节的涡流阀方案研究

介绍了一种固体发动机推力大小随机调节实现的方案－涡流阀方案，导出了涡流阀调节性能的相似准则方程；对涡流阀调节固体发动机静态特性和影响调节性能的各种主要因素进行了分析，指出了提出调节性能的途径，诸了模型发动机的推力调节。