Thermal ablation wear is a key factor in deciding the life of a rapid-fire-gun barrel.
热烧蚀磨损是决定速射火炮身管寿命的关键因素。
Objective To observe the effect of iodized oil for radiofrequency thermal ablation(RFA) of hepatic neoplasms by using a cluster array of ten separate electrodes.
目的观察用碘化油行肝动脉栓塞对集束电极射频热毁损治疗（RFA）肝癌疗效的影响。
Objective To observe the effect of iodized oil on radiofrequency thermal ablation (RFA) of hepatic neoplasms by using a cluster array of ten separate electrodes.
目的观察用碘化油行肝动脉栓塞对集束电极射频热毁损治疗（RFA）肝癌疗效的影响。
Such techniques include cryoablation, radiofrequency thermal ablation, microwave thermotherapy, high-intensity focused ultrasound, laser interstitial thermal therapy, and so on.
这些肿瘤消融技术包括冷冻、射频、微波、高强度聚焦超声、激光、等。
Objective To evaluate the clinical values of ultrasound guided percutaneous composite thermal ablation technique in the treatment of medium and large hepatocellular carcinoma(HCC).
目的评估超声引导复合热消融技术治疗中、大肝细胞癌（HCC）的应用价值。
This change may play an important role clinically in reducing postoperative local recurrence and metastasis, and strengthening the therapeutic effects of thermal ablation on tumor.
这对于减少肿瘤的局部复发和远处转移，增加热凝固治疗抗肿瘤疗效具有重要的临床意义。
Many results of oxyancetylene. ablation experiments and systematic thermal analysis of some composites have been calculated and analyzed in this paper.
对复合材料氧乙炔烧蚀试验及其系列热分析试验的结果进行了计算和分析。
The numerical results show that the transpiration control parameter can control the ablation and temperature of the thermal protection layer effectively.
数值计算证实，发汗控制参数能有效地控制热层烧蚀，同时也能有效地控制热层温度。
Objective to investigate the ablation range of Cool-tip radiofrequency generator and its thermal effect on liver cells, intrahepatic artery, vein and biliary duct.
目的研究射频热凝家兔肝组织的热效应范围，并观察肝细胞、肝内动脉、静脉及胆管组织的损伤情况。
Numerical simulation of high temperature thermal chemical ablation for carbon composite material was done and the ablation results were calculated.
对炭基复合材料在不同环境下热化学烧蚀过程进行了数值模拟，对烧蚀产物进行了计算。
The formulas to compute the charred thickness are derived based on its ablation mechanism and the methods to determine its design thickness arc given based on thermal protection for the chamber case.
根据内绝热层的烧蚀机理，推导出内绝热层炭优厚度计算公式；根据燃烧室壳体对热防护的要求，给出了确定内绝热层设计厚度的方法。
The local ablation of thermal insulation barrier in nozzle convergence region and of throat insert is analysed.
分析了喷管收敛段绝热层及喉衬的局部烧蚀问题；
According to the thermal shielding model of solid rocket motor, an approach of ablation heat shield design of end-burning grain with embedded wire was put forward in this paper.
根据固体火箭发动机绝热防护模型，提出了一种嵌金属丝端燃装药绝热层设计方法。
The principle of minimum free energy method was analyzed. The calculation method of thermal chemical ablation was studed.
运用最小自由能原理，研究了超高温热化学烧蚀的计算方法。
In clinical applications, it is important to select appropriate scanning speed to obtain both high ablation rates and minimal thermal injury.
因此，在临床应用上，应根据临床需要选择合适的扫描速度和辐射曝光量来获得大的消融率和小的热损伤。
The ablation mechanisms of components are particles erosion and mechanical denudation. Material failure is mainly caused by the thermal stress.
同时，材料所受到的热应力是引起材料失效的主要原因。
The effect on circumgyration of carbon grain and the ablation of nose-tip during re-entry of stratagem missile is analyzed according to thermal transfer theory, thermo-aerodynamics and N-S equation.
根据气动热力学、传热传质学、N - S方程，分析了战略导弹再入时端头帽烧蚀与碳颗粒的旋转效应，研究结果表明碳颗粒的旋转有利于防热。
The effect on circumgyration of carbon grain and the ablation of nose-tip during re-entry of stratagem missile is analyzed according to thermal transfer theory, thermo-aerodynamics and N-S equation.
根据气动热力学、传热传质学、N - S方程，分析了战略导弹再入时端头帽烧蚀与碳颗粒的旋转效应，研究结果表明碳颗粒的旋转有利于防热。
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