Advances in Solid Rocket-Ramjet Engine

 
       
  • 固体火箭-冲压发动机的研究进展

Advances in Solid Rocket-Ramjet Engine的用法和样例:

例句

  1. Computation of ablation of thermal-protection layer in solid rocket ramjet combustor
    固体火箭冲压发动机燃烧室热防护层烧蚀计算
  2. This paper established the mathematical models of integral solid rocket ramjet, aerodynamics and trajectory, and wrote the corresponding C++ code.
    本文建立了固体火箭冲压发动机性能计算、导弹气动性能计算和弹道仿真分析等分系统的数学模型,并编制了相应的C++计算程序模块。
  3. The secondary combustion of full-scale solid rocket ramjet was investigated by using the ground direct-connected experimental equipment with uncertainty evaluation.
    采用不确定度评定的地面直连冲压实验设备,对某全尺寸固冲发动机补燃室二次燃烧进行了实验研究。
  4. The numerical simulation of supersonic inlet internal turbulent flow of solid rocket ramjet assisted range projectiles was performed by 2-order implicit TVD.
    摘要应用二阶隐式TVD格式对固体火箭冲压发动机增程弹丸超音速进气道内部湍流流场进行了数值仿真。
  5. With zonal patched grid technology and second-order zonal solver method, the numerical simulation on inlet complex flow field of solid rocket ramjet assisted range projectiles with different struts shapes was made at different Mach numbers.
    摘要结合分区对接网格技术和二阶精度区域分解算法,对某冲压增程弹丸进气道在不同来流攻角和不同侧向支柱形状工况下的内外复杂流场进行了数值模拟。
  6. Interior Ballistics Calculation for Nozzleless Booster with Solid Propellant Rocket Ramjet Engine
    固体火箭冲压发动机无喷管助推器性能分析

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