the optimal location of heating tubes in greenhouse

1、

primary calculating model for integrated scramjet engine design

一体化超燃冲压发动机初步设计计算模型

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2、

three-dimensional massively parallel numerical simulation of kerosene-fueled scramjet

煤油超燃冲压发动机三维大规模并行数值模拟

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3、

research on flow characteristic of isolator in scramjet

超燃冲压发动机隔离段流动特性研究

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4、

on exploring design of hypersonic forebody/ inlet and isolator of integrated scramjet

超燃冲压发动机前体/进气道和隔离段气动设计

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5、

the liquid fuel atomization processes play an important role on scramjet performance.

使用液体碳氢燃料的超燃冲压发动机中的雾化是其工作中的一个重要环节，它对提高发动机的性能起着至关重要的作用。

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6、

variable geometry effects on the scramjet ignition and combustion

变几何喉道对超燃冲压发动机点火与燃烧性能的影响

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7、

analysis of design calculation methods of scramjet combustion chamber

超燃冲压发动机燃烧室设计计算方法的研究

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8、

the methodology for scramjet combustor performance analysis and evaluation is build up.

提出了超燃冲压发动机燃烧室的性能分析评价方法。

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9、

the scramjet is composed of inlet, isolator, combustor and nozzle.

超燃冲压发动机由进气道、隔离段、燃烧室和尾喷管组成。

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10、

test. in test on experimental studies of scramjet and its test facilities

论超燃冲压发动机试验研究及其试验设备

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11、

configuration effect analysis of scramjet combustor based on the integral balanceable method

基于综合平衡法的超燃冲压发动机燃烧室构型影响分析

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12、

effects of non-equilibrium chemical reaction flow on the performance of scramjet nozzle

化学非平衡流动对超燃冲压发动机尾喷管性能的影响

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13、

influence factor analysis of the mhd controlled scramjet inlet design

超燃冲压发动机磁控进气道设计影响因素分析

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14、

the influence of dual-cavity on pilot hydrogen distribution in scramjet combustor

超燃冲压发动机燃烧室中双凹腔对引导氢分布的影响

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15、

numerical research on subsonic-combustion and supersonic combustion modes in scramjet chamber

超燃冲压发动机燃烧室亚/超燃模态数值研究

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16、

experimental investigation of ignition technology in liquid hydrocarbon fueled scramjet combustor

碳氢燃料超燃冲压发动机点火技术试验

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17、

scramjet-powered air-breathing hypersonic vehicle has become a research focus nowadays.

以超燃冲压发动机为动力的吸气式高超声速飞行器，已成为现阶段的研究热点。

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18、

global one-dimensional finite volume euler equations coupled with chemical reactions are implicitly solved to simulate the reacting flowfield of the combustor of scramjet fueled by hydrogen or hydrocarbon.

本文采用隐式格式强耦合求解有限体积法离散的考虑化学反应的广义一维E uler方程，数值模拟氢或碳氢燃料超燃冲压发动机燃烧室的化学反应流场。

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19、

a three-dimensional numerical code has been developed to simulate supersonic reacting flows in scramjet combustor. the code employs an implicit, finite volume, lower-upper ( lu), and time-marching method to solve the complete navier-stokes and species equations in a fully coupled and efficient manner.

采用LU隐式方法强耦合求解有限体积法离散的完全N－S方程及组分方程，数值模拟超燃冲压发动机燃烧室内的化学反应流场。

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20、

mach 4 testing of scramjet inlet model

超燃冲压发动机4Ma进气道试验研究

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