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Aerodynamic heating of ballistic missile including the effects f gravity

机译:包括重力影响的弹道导弹的空气动力学加热

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摘要

The aerodynamic heating of a ballistic missile due to only convection is analyzed taking into consideration the effects of gravity. The amount of heat transferred to the wetted area and to the nose region has been separately determined, unlike A Miele's treatise without consideration of gravity. The peak heating rates to the wetted area and to the nose of the missile are also investigated. Finally four numerical examples are cited to estimate the errors, in heat transfers and heating rates to both wetted area and nose region of the missile, arising out of neglecting the gravitational forces.
机译:考虑到重力的影响,对仅由于对流引起的弹道导弹的空气动力学加热进行了分析。传给湿润区域和鼻子区域的热量已经分别确定,这与阿米勒的论文没有考虑重力有关。还研究了润湿区域和导弹机头的峰值加热速率。最后,列举了四个数值示例来估计由于忽略重力而引起的向导弹的湿润区域和机头区域的传热和加热速率的误差。

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