您要查找的是不是:
- Herb Chelner,Jim Buswell,Dan evans.Embedded sensors for monitoring solid propellant grain. 余宏发.;光纤传感器在固体发动机测试中的应用
- After having solved the aging problems of beams,the long term ag-ing effect of a solid propellent grain is also analyzed as an example. 在对梁的受拉伸与自重情形下的老化作了分析后,举例分析了真实固体火箭发动机药柱的长期老化效应。
- Viscoelastic stochastic finite element simulation of solid propellant grain with random Poisson's ratio 固体推进剂药柱泊松比随机粘弹性有限元分析
- Viscoelastic stochastic finite element simulation of solid propellant grain with random relaxation modulus 固体推进剂药柱松弛模量随机粘弹性有限元分析
- EXPERIMENTAL STUDY OF ANOMALOUS COMBUSTION IN SOLID PROPELLANT GRAIN WITH DEFECTS 含缺陷固体装药燃烧异常实验分析
- Nonprobabilistic Convex Set Theoretic Models for Structural Analysis of Solid Propellant Grain 固体推进剂药柱结构分析的非概率凸集合理论模型
- solid propellant grain 固体药柱
- Deformation of solid propellant grains under axial acceleration load 轴向过载下固体推进剂药柱变形研究
- The insulation layer, artificial debond layer and propellant grain in solid rocket motor chamber (SRM) are all polymer composite systems. 固体火箭发动机燃烧室内绝热层、人工脱黏层及推进剂药柱,均为高分子材料复合体系。
- Structural integrity analysis for the canular solid propellant grains subjected to temperature loading 温度载荷下带筋套管形装药结构完整性分析
- Near-Incompressible Viscoelastic Incremental Finite Element Analysis of Solid Propellant Grains 固体推进剂药柱的近似不可压缩粘弹性增量有限元法
- Numerical simulation for the axial deformation of solid propellant grains under the high acceleration shock 高加速度冲击下固体推进剂药柱轴向形变的数值模拟
- The fact proves that solid propellant could be possibly used as GDL fuel. 实验结果表明,固体推进剂可以 成为GDL燃料。
- FONG C W and MOY B K. Ballistic criteria for propellant grain fractur e[J]. J Ballistics 1982,6: 1410. 黄洪勇;王泽山.;两种工艺制造的低温感包覆火药性能的比较研究[J]
- The progress of the aging property of solid propellant were reviewed. 综述了国内外推进剂材料老化性能的研究进展。
- The crystallization of RDX from a tubular composite modified double-base propellant grain has been investigated with a scanning electron microscope. 用扫描电子显微镜研究了含RDX的管型改性双基推进剂的晶析情况。
- A mass of solid propellant. 块状燃料一块固体推进剂
- Solid propellant engine systems are basically less flexible in operation than liquid or hybrid propellant systems. 固体推进剂发动机系统的可调性基本上比液体或混合型的要差。
- We shall try by means of a highly simplified development to expose certain advantages and disadvantages of solid propellant rocket systems. 我们想通过相当简单的推导来试图阐明固体推进剂火箭系统的某些优缺点。
- solid propellant grains 固体推进剂