冲压发动机,ramjet
1)ramjet[英]["r?md?et][美]["r?md??t]冲压发动机
1.Investigation on a thrust vector design scheme oframjet;一种冲压发动机推力矢量设计方案研究
2.Improved BP Neural Network and its Application in Performance Predicting of Ramjet;改进BP神经网络在冲压发动机性能预测中的应用
3.A simplified method to analyze injecting phenomena and its application toramjet combustion chamber;冲压发动机燃烧室燃料喷射的简化计算方法研究
英文短句/例句
1.a machine for stamping out engine parts冲压发动机部件的机器.
2.Investigation of Flow Characteristics of Scramjet Isolator;超燃冲压发动机隔离段流动特性研究
3.Reliability assessment fer a type of ramjet engine;某型冲压发动机的可靠性评估(上)
4.Investigation on ground direct-connect test technology for water ramjet engine水冲压发动机地面直连试验技术研究
5.Analysis of Characteristics of Supersonic Speed Ramjet Isolator Inner Flow Fields超声速冲压发动机隔离段内流场分析
6.Numerical Simulation of Interior Flow Field in SFRJ固体燃料冲压发动机内流场数值模拟
7.Numerical Simulation of Flow Field of a Scramjet Combustor超燃冲压发动机燃烧室流场数值模拟
8.ON THE IGNITION PROCESS IN A MODEL SCRAM JET COMBUSTOR模型超燃冲压发动机内着火过程分析
9.Influence of Back Pressure on the Inner Flow Field in Scramjet Isolator反压对超燃冲压发动机隔离段内流场的影响
10.Reseach of Increasing Mixture in Supersonic Combustion Ramjet Engine Combustors;超燃冲压发动机燃烧室内增强混合机理研究
11.turbo-ram rocket engine涡轮冲压式火箭发动机
plete athodyd冲压式空气喷气发动机
13.automatic punching machine(冲压机用语) 自动冲床
14.Analysis of flux-adjustable and ramjet-nozzle-adjustable solid ducted rocket可调冲压喷管变流量固冲发动机工作特性分析
15.ramjet exhaust nozzle冲压式喷气发动机排气喷管
16.supersonic combustion ramjet超音速燃烧冲压喷气发动机
17.subsonic combustion ramjet亚音速燃烧冲压喷气发动机
18.liquid-fuelled ramjet engine液体燃料冲压喷气发动机
相关短句/例句
ramjet engine冲压发动机
1.Design method of regulating rule forramjet engines based on similarity parameters;基于相似参数的冲压发动机调节规律设计方法(英文)
2.Analysis of the powdered carbon combustibility in secondary combustion chamber for rocketramjet engine;碳粉燃料在火箭冲压发动机补燃室内燃烧特性的分析
3.Numerical simulation of theramjet engine separation flow;冲压发动机转级流场数值仿真研究
3)scramjet[英]["skr?md?et][美]["skr?m,d??t]冲压发动机
1.Development of supersonicscramjet inlet;冲压发动机超声速进气道研究进展
2.Thescramjet,the engine of hypersonic aircraft,is a key apparatus.对在高超声速冲压发动机燃烧实验研究中,使用燃烧式加热器得到高焓、高压、高超音速气流时,实验介质中带入的水组分进行了模拟计算。
3.The performance of a MHD-Arc-Scramjet combined cycle engine is analyzed by investigating the effect of energy-bypass system on the engine specific thrust and presenting the difference of the specific thrust between the MHD-Arc-Scramjet combined cycle engine and a conventionalscramjet.以MHD-Arc-Scramjet联合循环发动机为对象开展性能分析,探讨了能量旁路系统对发动机性能的影响,给出了MHD-Arc-Scramjet联合循环发动机相对于传统冲压发动机的单位推力差异。
4)Ramjet engine冲压喷气发动机
5)ramjet assistant range冲压发动机增程
6)scramjet[英]["skr?md?et][美]["skr?m,d??t]超燃冲压发动机
1.Application of flamelet model for the numerical simulation ofscramjet;火焰面模型在超燃冲压发动机数值模拟中的应用
2.Numerical Simulation of Liquid Spray Atomization in Scramjet Combustor;超燃冲压发动机燃烧室液体射流雾化数值模拟
3.Interaction of shock/boundary layers in ascramjet inlet;超燃冲压发动机进气道内激波/边界层干扰研究
延伸阅读
冲压发动机利用高速迎面气流进入发动机后减速使空气增压的航空发动机。冲压发动机通常由进气道(又称扩压器)、燃烧室和喷管组成。航空器飞行时迎面气流在通过进气道的过程中将动能转变为压力能,经压缩后的空气进入燃烧室与燃料混合进行等压燃烧,生成的高温燃气在喷管中膨胀加速后排出,产生推力。冲压发动机结构简单,重量轻,成本低。在飞行马赫数大于3的条件下使用,有较高的经济性。它的缺点是不能自行起动,须用其他发动机作为助推器,俟飞行器达到一定飞行速度后才能有效工作。冲压发动机按应用范围分为亚音速、超音速和高超音速3种:①亚音速冲压发动机:使用扩张形亚音速进气道和收敛形喷管,以航空煤油作燃料。飞行时,空气增压比不超过1.89,发动机热效率低。随着飞行速度的减小,效率迅速降低。一般在飞行马赫数小于 0.5时不能使用。亚音速冲压发动机可用于亚音速航空器如靶机。②超音速冲压发动机:飞行速度在马赫数1~6之间。为了减少气流在减速增压过程中的损失,采用多激波系的超音速进气道,进气道出口气流是亚音速的。发动机使用航空煤油或高密度烃类燃料。燃烧室用火药点火器或电火花塞点火。高温燃气通过收敛形或收敛扩散形喷管加速后喷出。超音速冲压发动机用于超音速靶机和地空导弹。③高超音速冲压发动机:使用碳氢燃料或液氢燃料,飞行马赫数为5~16。燃料在超音速气流中燃烧,能减少气流压缩和膨胀损失,降低气流静温和静压,减轻发动机结构负荷。高超音速冲压发动机研制的关键是解决边界层分离、气动加热和燃烧不稳定性问题。除使用液体燃料的冲压发动机外,还有使用含镁粉或铝粉等富燃料药柱的固体冲压发动机和使用核能加热空气流的核冲压发动机等。