... reentry attitude dynamics 再入姿态动力学 reentry body 再入体 reentry capsule 再入（大气层）舱 ...
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Some engineering correlations have been developed to predict the fluctuating pressure distribution on the sphere biconic shape reentry vehicles surface in supersonic/hypersonic flow field. Utilizing the pressure distribution,we achieved a series of reasonable results comparing with test data.
本文根据超声速和高超声速流动特征分析了球头双锥再入体的表面脉动压力环境特性 ,并根据超声速和高超声速流动情况下球头双锥的表面压力分布给出一套预测球头双锥再入体表面脉动压力分布的工程估算公式。
参考来源 - 球头双锥再入体表面脉动压力环境的分析与预测·2,447,543篇论文数据，部分数据来源于NoteExpress
文中着重叙述了再入体滚转共振和小不对称气动力问题的研究结果和存在问题。
Research results of the re-entry body in rolling resonance and small asymmetrical aerodynamic force as well as existential problems are emphatically described. It indicates that to determine rand…
建立了再入体再入大气层形成的尾迹的工程模型，并运用边界层理论求解二维等压湍流尾迹流动。
An engineering model for hypersonic reentry body trail is established in this paper, and a calculation is performed by using boundary layer theory.
本文简要介绍了再入体六自由度控制系统半实物仿真的系统结构与软件系统设计，并探讨了相应的仿真技术途径。
In this paper, system structure and software design of reentry vehicle Sir -dof semi physical simulation are introduced briefly, and corresponding simulation technical methods is discussed.
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