增压比的英文

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"增压比"怎么读用"增压比"造句

英文翻译手机版

boost ratio
rate of pressurization
rate of supercharging
supercharge ratio

"增压"英文翻译 pressurize; supercharge; pre ...
"比"英文翻译 2
"增压器增压比" 英文翻译 : supercharger ratio
"喘振增压比" 英文翻译 : surge pressure ratio
"风扇增压比" 英文翻译 : fan compression ratio
"压缩增压比" 英文翻译 : compressor pressure ratio
"总增压比" 英文翻译 : overall compression ratio; overall pressure ratio; total compression ratio
"鼓风机增压比" 英文翻译 : blower ratio
"进气道增压比" 英文翻译 : inlet compression ratio
"压气机增压比" 英文翻译 : compressor pressure ratio
"压缩机增压比" 英文翻译 : compressor pressure ratio; compressorpressureratio
"压缩器增压比" 英文翻译 : compressor pressure ratio
"增压比指示器" 英文翻译 : pressure-ratio gauge
"低增压比发动机" 英文翻译 : low-pressure engine
"发动机循环增压比" 英文翻译 : engine cycle pressure ratio
"高增压比发动机" 英文翻译 : high-pressure engine
"最大有效增压比" 英文翻译 : highest useful compression ratio
"高增压比的轴向式压缩器" 英文翻译 : high-pressure ratio axial flow compressor
"压比" 英文翻译 : compression ratio; pressure ratio
"增压" 英文翻译 : pressurize; supercharge; pressure boost◇增压泵 blower pump; [航空] booster pump; 增压表 [航空] boost gauge; 增压舱 pressure cabin; 增压服 pressure suit; 增压站 booster station; 增压装置 supercharging device; 增压作用 pressurization; supercharging; 增压座舱 positive pressure cabin; sealed cabin
"变压比" 英文翻译 : ratio of transformation; ratio of transformer; transformation ratio; transformer ratio; transformer-ratio
"差压比" 英文翻译 : differential pressure ratio
"冲压比" 英文翻译 : ram pressure ratio; ram ratio
"电压比" 英文翻译 : ratio voltage; ratio-voltage; voltage ratio method
"锻压比" 英文翻译 : ratio of forging reduction

例句与用法

Compressor pressure ratio
压气机增压比
It is shown that when the exit area of secondary nozzle and the fuel / oxidizer ratio is fixed , the increase of mass flow rate of secondary flow lead to the decrease of velocity of mixed flow , and increase of total mass flow rate . the synthetical result of these two phenomenon cause the increase of thrust of rocket ejector , but the increasing magnitude is relatively small , indicating that these is no necessary to claim large bypass ratio in rocket ejector design . in the comparison between two configurations , the typical one has better performance , indicating the importance of pressure ratio
结果表明：在固定二次喷管出口面积和氧燃比的条件下，二次流(引射空气流)流量的增加引起混合气体出口速度的下降和总流量的增加，二者综合作用使发动机推力增加，但增幅不大，表明在设计发动机结构和工作参数时，不必过分追求大的引射系数；两种结构的性能对比分析表明了增压比对引射火箭性能的提高具有重要意义；对引射火箭的热力循环分析同样表明，增压比对于提高发动机性能非常关键。