afterburning
英
美
n. 加力燃烧；复燃；补充燃烧
双语例句
- You'll eat so much your belly'll be like a barrel.
你会吃得肚子鼓鼓的，像个大酒桶。 - With the deepening of reform and opening up for the perfect modern enterprise system, Rugao Afterburning silk plant for conversion to private limited liability company.
随着改革开放的深入为完善现代企业制度，如皋加力丝绵厂改制为私营有限责任公司。 - We are now a daily Afterburning milk, cod liver oil a day, may I ask to increase the you?
我们现在是每天一粒乳加力，两天一粒鱼肝油，请问要增加吗？ - Afterburning macro-control will, of the reasons is that the real estate market is the rapid growth of the huge financial risks.
加力宏观调控会，原因是，房地产市场的快速增长的巨大金融风险。 - I plant has a long history, is the early Rugao Afterburning silk plants, their products have been selling domestic and foreign markets.
我厂具有悠久的历史，是早年的如皋加力丝绵厂，其产品一直畅销国内外市场。 - An experimental method for simulating oxygen-rich condition in afterburning chamber of solid ducted rocket ( SDR) was developed for insulation ablation investigation.
发展了一种能模拟固体火箭冲压发动机补燃室富氧环境并用于绝热层烧蚀研究的试验方法。 - The results show that developing process of mixing in afterburning chamber is different along with the change of fuel-gas jetting modes. It is uncertain that the method to improve integral mixing degree in chamber will raise head-end mixing degree.
结果表明，燃气喷射方式不同，掺混在补燃室中的发展过程也不同，提高补燃室内整体掺混度的方法，不一定能提高头部的掺混度； - Analysis of Overheater Excess Temperature in Exhaust-heat Afterburning Boiler
余热补燃锅炉过热器超温问题分析 - Gas produced by conventional gas generator, air and oxygen ( nitrogen) were mixed, and some parameters including pressure, flow, temperature and oxygen-rich degree in afterburning chamber were adjusted by controlling flow.
用常规燃气发生器产生的燃气，与补进的氧气（氮气）、空气混合，通过控制流量，模拟固冲发动机补燃室内的压强、流量、燃气温度和富氧度等参数。 - The way improving afterburning efficiency was theoretically found.
该研究从理论上找到了提高补燃效率的途径。 - Effects of the air inlet angle and jet number on mixing flow in the afterburning chamber of solid rocket ramjet
喷口数与进气道角对固冲发动机补燃室气流掺混的影响 - Nonlinear optimal control of turbofan engine afterburning process
涡扇发动机加力过程非线性最优控制研究 - An identification technique was presented for estimating the impurity level in propellant and the properties of exhaust afterburning, which can not be measured simply by experiment.
提出用参数辨识确定推进剂中钾、钠杂质含量以及后燃对喷焰微波衰减影响程度的方法。 - An experimental study of Mach disk affecting afterburning in high underexpanded muzzle jet
膛口高度欠膨胀射流中马赫盘对二次着火影响的实验研究 - The main object of this paper is that the representative comprehensive characteristics of similar parameters at maximum and afterburning conditions of engine, subsonic and transonic flight, i. e. of various maneuvers.
本文旨在通过各种机动飞行，荻得最大状态、加力状态、亚音速和跨音速典型的相似参数综合特性线，利用这些曲线可计算飞机大速度、稳定盘旋，跃升拉起和盘旋上升等一些典型性能。 - Numerical Simulation of the Influence of Nozzle Area Control Accuracy on Turbofan Afterburning Performance
喷管面积调节精度对某型涡扇发动机加力性能影响的数值仿真 - Optimization control of minimum fuel consumption at aero-engine afterburning condition
航空发动机加力状态最小油耗优化控制 - Dispersity of gas flow can be enhanced and afterburning efficiency can be improved by increasing primary nozzle numbers and nozzle expansion ratio.
增加一次喷嘴的数目和加大喷嘴的扩张比增加了燃气的分散性，提高了补燃效率。 - The results show that the increment of oxidizer inlet expansion is favorable for efficiency and stabilization of the motor, and the increase of length of the afterburning chamber can raise the average burning temperature and improve the combustion efficiency.
结果表明，增加氧化剂入口突扩段有利于发动机稳定工作和充分燃烧，增加补燃室长度可以提高发动机平均燃烧温度，使燃烧更加充分。 - The establishment of mathematical model of engine control system and Simulation Research of afterburning dynamic characteristics
发动机控制系统数学模型的建立及加力动态特性的仿真研究 - A method," gross thrust model", is developed to determine gross thrust of jet engine and afterburning turbofan engine in flight testing.
提出了一种飞机飞行中发动机推力测定的总推力模型。 - Bubble Chamber But the effect can vary for different afterburning chamber structures.
但对不同的补燃室结构，二次燃烧效率随补燃室长度变化的趋势不尽相同。 - The results show that the process of radiation of firelight from explosion consists of two phases: detonation and afterburning.
结果表明，凝聚相炸药的爆炸发光过程由爆炸和后燃两阶段组成。 - By using Renault averaged Navier-Stokes equation and κ-ε turbulent combustion model, the mixing and combustion flow-field in afterburning chamber of a choked solid ramjet was numerically simulated.
用雷诺平均N-S方程和κ-ε双方程湍流模型，对壅塞式固体火箭冲压发动机补燃室内的掺混与燃烧流场进行了数值模拟。 - The suppression technology of afterburning on solid rocket motor exhaust
固体火箭发动机排气二次燃烧的抑制技术 - Parameters identification of alkali metal impurities of solid propellant and properties of exhaust afterburning
固体推进剂碱金属杂质及喷焰后燃效应的参数辨识研究 - Contrast study on cold-flow mixing effect and combustion efficiency of afterburning chamber of solid rocket ramjet
固冲发动机补燃室冷流掺混效果与燃烧效率对比研究 - The results showed that pressure changes caused by the afterburning and pumping components in fuel system were the main reason to lead to cavitation erosion. Phase-select and hollow out behaviors had been observed on the eroded surface.
结果表明，燃油系统中加力及泵油部件导致的高压高速航空煤油压强快速变化是造成空蚀的主要原因，空蚀过程中通常还伴有显著的相选择行为及由其引发的镂空效应。 - The simulation includes high-altitude starting and the ground starting in different environments such as high/ low temperature or plateau. The acceleration and deceleration process in above-idle process and afterburning process are also simulated.
模拟了地面高温、低温、高原三种不同环境下的地面起动；空中风车起动和空中起动机带转起动两类高空起动；慢车以上加减速过程和加力过程。 - The blast power of TBE was higher due to the enhancement of afterburning to shock wave.
由于后续燃烧对冲击波的增强作用，使药剂具有较高的爆炸威力。