1) aerothermal ablation
气动热烧蚀
2) aerodynamic ablation
气动烧蚀
1.
The aerodynamic ablation of hypersonic penetrator shell at angle of attack is studied by using the axisymmetric analog method, making use of comparability theory and basing on small cross flow hypothesis.
该文采用“轴对称比拟”的研究方法,运用相似性理论,基于小横向流假设,研究了有攻角高超声速穿甲弹的气动烧蚀。
3) ablation-aerodynamic interference
烧蚀-气动力干扰
4) Thermal ablation rate
热烧蚀率
补充资料：弹头烧蚀(见弹头防热)
弹头烧蚀(见弹头防热)
warhead ablation
dantou shaoshi弹头烧蚀(warhead的lation)见弹头防热。
说明：补充资料仅用于学习参考，请勿用于其它任何用途。
参考词条