1) Ablation mode
烧蚀模式
1.
Using high power pulse TEA-CO-2 laser and Ktype thermocouple,the temperature distribution on a parabolic reflector and the temperature response under different pulse number and atmospheric pressure were investigated in air-breathing and ablation mode,respectively.
在激光脉冲个数确定的条件下,大气呼吸模式的温度随气压的减小先增大后减小,出现一个峰值;烧蚀模式则随气压的减小而增大。
2) Ablative mode
烧蚀模式
1.
Adopting the numerical method of differential equation to solve the motion equations of micro-aircraft propelled by pulse ground based laser,the flight characteristics of aircraft in air-breathing mode,ablative mode and combining air-breathing mode with ablative mode are discussed.
采用微分方程数值解法计算地基脉冲激光推进轻型飞行器的运动方程,分析了大气呼吸模式、烧蚀模式以及两种模式相结合方式下飞行器的飞行特点。
3) Rocket ablation mode (RAM)
火箭烧蚀模式
4) ablative rate
烧蚀模型
1.
The mass ablative rate of C/TaC/C composites is ultimatel.
根据TaC和C/C复合材料的物理化学性质及烧蚀环境推测C/TaC/C复合材料的烧蚀机理,并对其抗侵蚀机理及剥蚀进行了预测分析,在分析C/TaC/C复合材料烧蚀机理的基础上建立其烧蚀模型。
6) wallrock alteration model
蚀变模式
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