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ramjet

美 ['ræmdʒet]英 ['ræmdʒet]

na.冲压喷气(发动机)
网络冲压发动机；冲压式喷气发动机；冲压喷气发动机

复数：ramjets

ramjet

ramjet

英-汉英-英网络释义

ramjet

na.

1.冲压喷气(发动机)

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The propellant which has higher density special impulse can be applied into ramjet which has no nozzle .

具有较高密度比冲的高能推进剂可用于无喷管推进的冲压发动机中。

3

MODEL 79 Meanwhile , McDonnell continued to seek an outlet for the principles and design simplicity developed in the XH-20 ramjet helicopter .

模型 79 与此同时，麦继续寻求出路的原则和设计开发的简单新华 -20 喷气直升机。

5

China already has such segmented solid rocket motor and ramjet capabilities today, but scramjets are a much greater challenge .

中国已经拥有这种分离式火箭助推器和冲压发动机技术，但超音速燃烧冲压发动机是一个更大的挑战。

7

Ramjet engine is ideal propulsive equipment for new supersonic missile , and supersonic inlets are important components .

冲压发动机是新一代超声速导弹理想的动力装置，超声速空气进气道是它的一个重要部件。

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The influences of mass warp, aerodynamic resistance warp and solid rocket-ramjet engine thrust warp on the flight velocity are analyzed .

研究了靶弹质量偏差、气动阻力偏差和冲压发动机推力偏差对飞行速度的影响。

12

Ramjet combustor with cavity as flameholder has simple configuration and excellent flame hold characteristic .

凹腔作为火焰稳定器具有结构简单、火焰稳定能力强的特点。

13

Ramjet engines have traditionally used liquid fuel which is mixed with atmospheric air and burned to provide thrust for high-speed flight .

传统的冲压喷气发动机使用液体燃料并与大气中的空气混合燃烧，以提供高速飞行的推力。

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the simulation model of operation process of solid fuel ramjet was established .

建立了固体燃料冲压发动机工作过程仿真模型。

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These include a combined solid-motor, ramjet-powered PL-21.

这些包括以混合固体燃料冲压发动机为动力的 PL-21 。

19

The SH-5 was originally scheduled to carrying the YJ-1 (C-101) supersonic ramjet -powered anti-ship missile for surface strike role .

5 本来预定为水面打击角色携带 YJ-1 （C-101 ）超音速冲压发动机反舰导弹。

21

Ignition Experimental Study of a Variable Geometrical Throat Dual-mode Ramjet

几何可调喉道双模态冲压发动机点火过程试验研究

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Experimental study of a variable-area propelling nozzle dual-mode ramjet

可调喷口双模态冲压发动机试验研究

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Study of the influence of environment to the performance of ramjet ignition device

环境对冲压发动机烟火点火器性能影响研究

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Numerical Simulation on the Inlet Complex Turbulent Flow of Ramjet Assisted Range Projectiles

冲压增程弹丸进气道复杂湍流流场数值仿真

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Numerical Simulation on Inlet Complex Flow of Ramjet Assisted Range Projectiles with Zonal Method

冲压增程弹丸进气道内外流场分区数值模拟

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Numerical study of the throttle characteristic about the ramjet inlet and mixing section

冲压发动机进气道和掺混段节流特性数值研究

28

Genetic algorithm applied to integral design optimization of missile propelled by solid rocket ramjet

固体火箭冲压发动机导弹一体化遗传算法优化设计

29

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

30

Application of TTM grids on the research of inlet complex flow of ramjet assisted range projectile

应用 TTM 网格研究冲压增程弹丸进气道内外流场

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