Numerical Calculation of Dynamic Stability Derivatives for Capsule-type Re-entry Vehicle

机译：胶囊式再入车辆动力学稳定性导数的数值计算

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A harmonic oscillation method for solving unsteady Euler equation and a forced oscillation method for solving unsteady TLNS equation is presented to calculate dynamic stability derivatives for hypersonic flow over blunt body. These two methods are may applied to calculating the damping-in-pitch, damping-in-yaw and damping-in-roll derivatives for capsule-type re-entry vehicle.

机译：提出了求解非定常Euler方程的简谐振动方法和求解非定常TLNS方程的强制振荡方法，以计算钝体上超音速流的动力稳定性导数。这两种方法可用于计算胶囊式再入车辆的俯仰阻尼，偏航阻尼和侧倾阻尼导数。

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《International symposium on computational fluid dynamics;ISCFD'97》|1997年|p.750-756|共7页
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Zhang Lumin; Liu Wei; Yuan Xianxu; Zhang Hanxin;
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中图分类航空;
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Numerical Calculation of Dynamic Stability Derivatives for Capsule-type Re-entry Vehicle

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