喷管结构的英文

• nozzle structure

• "结构"英文翻译    structure; composition; cons ...
• "管结构" 英文翻译 :    tube design; tubular construction; tubular structure
• "钢管结构" 英文翻译 :    steel pipe construction; steel tube construction; steel tubular structure; steel-pipe co truction; steel-pipe construction; steel-tube construction; tubular structure
• "晶体管结构" 英文翻译 :    transistor arrangement; transistor construction; transistor structure
• "螺线管结构" 英文翻译 :    solenoid structure
• "密排管结构" 英文翻译 :    tangent tube construction
• "筛管结构" 英文翻译 :    screen construction
• "微管结构" 英文翻译 :    micro-tubular structure
• "维管结构" 英文翻译 :    vasculature
• "铜管结构馈线" 英文翻译 :    copper pipe feeder
• "圆筒排管结构" 英文翻译 :    barrel-calandria
• "凹腔型微波管结构" 英文翻译 :    reentrant
• "横向晶体管结构" 英文翻译 :    lateral transistor structure
• "双层组合套管结构" 英文翻译 :    pipe in pipe casing
• "管结" 英文翻译 :    pipe hitch
• "电荷耦合 场效应晶体管结构" 英文翻译 :    charge coupled fet
• "神经血管结构发育不全" 英文翻译 :    hypoplasia of musculotendinous structures
• "椎管结构化学松解术" 英文翻译 :    chemolysis of spinal canal structure
• "喷管" 英文翻译 :    atomizer device; atomizer pipe; augmenter tube; blast tube; duct; effuser; exhaust cone assembly; injection pipe; inlet bend; inlet elbow; jet pipe; jet tube; lance; metal nozzle; mouthpiece; nozzle pipe; nozzle tube; rod pipe; spray bar; spray pipe; sprayer nozzle; thrust jet
• "管结点" 英文翻译 :    tubular joint
• "管结合" 英文翻译 :    union coupling; union joint
• "胆管结石" 英文翻译 :    calculus of bile duct
• "胆管结扎钳" 英文翻译 :    bile duct ligature forceps; cystic duct and ligature clamp
• "胆囊管结石" 英文翻译 :    calculus of cystic duct
• "胆总管结石" 英文翻译 :    calculus of common bile duct; common duct stones

• The machining , installation , debug of the nozzle are completed after its design , and the finial running results of the nozzle are provided
  在喷管结构设计完成后进行喷管加工、安装、调试,最终给出喷管实际调试结果。
• Equality design method was used in numerical simulations , and multiobjective optimization method was used to design the scramjet nozzle configuration
  通过均匀设计法设计仿真算例,并通过多目标优化设计方法设计出了性能较好的喷管结构。
• The influence of primary flow and secondary nozzle geometry on ejector effect and thrust was investigated , and the approach to increase thrust of rocket ejector was found gradually
  研究了一次流参数和二次喷管结构对引射效能和发动机推力的影响，找到了逐步提高推力的措施。
• ( iii ) the structure design of the nozzle is completed according to coordinate data of the nozzle contour . the airproof design problem and the throat - cooling problem are mainly solved during the structure design
  (三)根据喷管型面坐标数据进行喷管结构设计,在喷管结构设计中着重解决密封设计和喉道冷却等问题。
• Variation tendency of nozzle gap and contact stress was obtained in terms of multi - time computational results , and some modification suggestions , which are available for designers of solid rocket motor nozzle , were presented by the tendency
  综合多个时刻的计算结果得到发动机工作过程中喷管结构缝隙和接触应力的变化趋势，并据此对设计缝隙提出了修改意见，结果可为发动机喷管设计提供参考。
• The effects of such elements as primary flow total pressure , flow rate , degree of fuel rich , nozzle structure , flying speed and secondary combustion on ejecting mode performance were researched . it was found that thrust augmentation can be achieved on the condition that the flying mach number is above 0 . 7 . to deeply analyze thrust augmentation mechanism in low speed range , the research was further continued by changing secondary combustion organization and aft - body configuration
  研究了一次流总压、流量、富燃程度、喷管结构、二次流来流速度、二次燃烧组织对引射模态性能的影响，发现实验样机构型在0 . 7ma以上的飞行条件下可以获得推力增强，而在0 . 7ma以下无推力增强。