ramjet

ramjet

1. ramjet engine

n. 冲压式喷气发动机

2. ZHANG Wei,ZHU Hui,FANG Ding-you,et al.Fuel-rich propellant fuel mass flow solid for adjustable ramjet engine[J].Journal of Propulsion Technology,1999,20(5):95-98.

[5]张炜,朱慧,方丁酉,等.用于燃气流量可调固冲发动机的富燃推进剂[J].推进技术,1999,20(5):95-98.

3. On top was an 18-ft diameter, twin-bladed rotor carrying a 10-lb ramjet burner at each of the tips.

上方是一个18英尺长，直径双转子叶片进行了10磅冲压发动机燃烧在每个秘诀。

4. 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。

5. Numerical simulation on turbulent flow in ramjet chamber with central inlet swirl injection

中心进气旋转射流冲压燃烧室湍流流动数值模拟

6. In order to verify the ignition and combustion performances of the metal-powder fuel ramjet,preliminary direct-connected test for the motor was carried out.

为了检验金属粉末燃料冲压发动机的点火及燃烧特性,对设计的发动机进行了初步的直连式试验研究。

7. To investigate the mechanism of scalar transport, the methane fuel concentration and temperature transport and diffusion in ramjet dump combustor was simulated by large eddy simulation.

为弄清突扩燃烧室内标量输运机理,采用大涡模拟方法数值模拟了几何结构简化的冲压发动机突扩燃烧室内湍流流动中燃料浓度以及温度等标量的扩散和输运过程。

8. The internal combustion engine (Otto cycle) ， Diesel cycle ， Brayton cycle ， Brayton cycle for jet propulsion; the ideal ramjet

了解并掌握内燃机和燃气轮机装置的实际工作循环可抽象为理想气体的热机循环。

9. Influence of air mass flow rate ratio on combustion efficiency of solid rocket ramjet with two air inlets

二次进气流量比对固冲发动机燃烧效率的影响

10. ramjet mode

亚燃模态

11. subsonic ramjet

亚音速冲压喷气发动机

12. subsonic combustion ramjet

亚音速燃烧冲压喷气发动机

13. According to working mechanism of water ramjet,operation principle of the gas generator water ramjet was put forward.

从水冲压发动机的工作机理出发,提出了适合开展发动机原理性研究的燃气发生器式水冲压发动机的工作原理。

14. Low Volume Ramjet

低容量喷气引擎

15. Advanced ramjet technologies are also important for scramjet development, and the Chinese have been active in this area for decades.

先进亚燃冲压技术对于超燃冲压技术至关重要，而中国数十年来在这一领域一直很活跃。

16. Influence of Inlet Conditions on Thrust and Specific Impulse of Solid Fuel Ramjet

入口条件对固体燃料冲压发动机推力和比冲的影响分析

17. Full-Scalc Liquid Fuel Ramjet Combustor Tests.

全尺寸液体冲压发动机燃烧室试验。

18. Keywords applied chemistry;fuel-rich propellant;boron;energy;solid rocket propellant ramjet;

关键词应用化学;富燃料推进剂;硼;能量;固体火箭冲压发动机;

19. ramjet engines

冲压发动机

20. The ramjet engine has many advantages such as simple structure, light weight, little volume, big ratio of pushing and gravity, low cost, and etc.

冲压发动机具有结构简单、重量轻、体积小、推重比大、成本低等一系列优点。

21. ramjet cycle

冲压发动机循环

22. ramjet control system

冲压发动机控制系统

23. A simplified method to analyze injecting phenomena and its application to ramjet combustion chamber

冲压发动机燃烧室燃料喷射的简化计算方法研究

24. ramjet stage

冲压发动机级

25. Flow rates calculation of combustion heater for ramjet test facility

冲压发动机试车台空气燃烧加热器流量参数计算

26. Viscous pressure forming of super-alloy super-thin wall corrugated parts applied to ramjet engine

冲压发动机超薄壁波纹形件的粘性介质压力成形

27. ramjet inlet

冲压发动机进气道

28. 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

29. ramjet duct

冲压发电机

30. ramjet performance

冲压喷气发动机性能

31. ramjet helicopter

冲压喷气式直升飞机

32. ramjet propulsion

冲压喷气推进 冲压式发动机 冲压式喷气发动机

33. ramjet assisted range projectile

冲压增程弹

34. 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

35. ramjet extended range projectile

冲压增程炮弹

36. Analysis of the Engine Performance for the Ramjet Extended Range Projectile

冲压增程炮弹发动机工作性能分析

37. ramjet sustainer

冲压式主发动机

38. ramjet speed

冲压式发动机速率

39. Ramjet: Air-breathing jet engine that operates with no major moving parts.

冲压式喷射发动机:工作时没有重要运动部件的一种喷射发动机。

40. ramjet exhaust nozzle

冲压式喷气发动机排气喷管

41. Air-breathing gas dynamic laser is developed as a new conception based on ramjet and gas dynamic laser.

冲压式气动激光器是在冲压发动机和气动激光器的基础上发展起来的一个新概念。

42. 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

43. Applications of gas generator in ramjet direct-connect test facility

加热器在冲压发动机试验技术中的应用研究

44. A simple, essentially tubular jet engine, such as a ramjet.

压式喷气发动机一种简单的，主要为管道式的喷气发动机，如喷压式发动机

45. dual-mode ramjet engine

双模态冲压发动机

46. Keywords Dual-mode ramjet engine;Supersonic combustion;Ignition process;Mode transition;Performance analysis;Combustion performance;Theoretical analysis;Experimental investigation;Numericalsimulation;

双模态冲压发动机;超声速燃烧;点火;模态转换;性能分析;燃烧室性能;理论分析;试验研究;数值模拟;

47. dual-combustion ramjet

双燃烧室发动机

48. Keywords engine;Internal-Rotor Burnt Rotating Ramjet （IRBRR）;ram-compressed rotor;ram-compressed;moving shock wave;numerical simulation;experimental study;

发动机;内置燃烧室旋转冲压发动机;冲压转子;冲压压缩;运动激波;数值模拟;实验研究;

49. 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

50. Numerical simulation of reacting fuel-rich flow field laden with boron particle in the ramjet combustor

含硼贫氧燃气补燃室反应流场研究

51. 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

52. So it is of very important science meaning and practice value to simulate the circle flow field of the ramjet shell.

因此,对冲压增程炮弹绕流流场的研究具有重要科学意义和实用价值。

53. solid propellant ramjet

固体冲压发动机

54. ducted solid rocket ramjet

固体火箭冲压发动机

55. Keywords solid fuel rocket ramjet;boron-based fuel-rich propellants;propellant combustion;combustion efficiency;

固体火箭冲压发动机;含硼富燃料推进剂;推进剂燃烧;燃烧效率;

56. Keywords Solid Rocket Ramjet;Secondary Combustion Chamber;Boron-Based Propellant;Two Phase Flow;Numerical Simulation;Connected-Pipe Ramjet Test;Temperature Measurement;Response Surface Method;

固体火箭冲压发动机;补燃室;含硼推进剂;两相流;数值模拟;直连式试验;辐射测温;响应面方法;

57. Keywords solid rocket ramjet;afterburning chamber;boron particles;two-phase flow;combustion flow field;

固体火箭冲压发动机;补燃室;硼粒子;两相流;燃烧流场;

58. A CAD System for Solid Propel? Lant Ramjet Rocket Motor

固体火箭冲压发动机一体化CAD系统设计

59. Ground test equipment and measurement-control system of solid rocket- ramjet engines

固体火箭冲压发动机地面试验装置及测控系统

60. Interior Ballistics Calculation for Nozzleless Booster with Solid Propellant Rocket Ramjet Engine

固体火箭冲压发动机无喷管助推器性能分析

61. Gas Flow Control Technique of Rocket Ramjet

固体火箭冲压发动机燃气流量调节技术与实验研究

62. Computation of ablation of thermal-protection layer in solid rocket ramjet combustor

固体火箭冲压发动机燃烧室热防护层烧蚀计算

63. Experimental study of mixing flow in afterburning chamber of solid rocket ramjet in cold flows

固体火箭冲压发动机补燃室冷态流场实验研究

64. Numerical simulation of mixing and combustion flow field in afterburning chamber for solid rocket ramjet

固体火箭冲压发动机补燃室掺混与燃烧流场数值模拟

65. solid - fuel ramjet

固体燃料冲压发动机

66. THEORETICAL ANALYSIS OF FLOW IN THE COMBUSTION CHAMBER OF A SOLID FUEL RAMJET

固体燃料冲压发动机燃烧室流动分析

67. Flight Performance Analysis of the Solid Fuel Ramjet

固体燃料冲压发动机飞行性能分析

68. solid ramjet

固冲发动机

69. Contrast study on cold-flow mixing effect and combustion efficiency of afterburning chamber of solid rocket ramjet

固冲发动机补燃室冷流掺混效果与燃烧效率对比研究

70. Solid fuel ramjet - assisted projectile

固冲增程炮弹

71. Building on its ramjet experience, China is embracing the much more difficult task of developing Mach 5 air vehicle concepts in which propulsion and aerodynamics are highly coupled.

在其冲压发动机发展经验基础之上，中国着手于更为艰巨的5马赫高超音速概念飞行器的开发，推进技术和空气动力将高度耦合。

72. choked solid rocket ramjet

壅塞式固冲发动机

73. recombination ramjet engine

复合冲压式发动

74. recombination ramjet

复合式冲压空气喷气发动机

75. practical ramjet

实用冲压式空气喷气发动机

76. The capability of turbo-pump working in variable conditions is required and important for pump-pressurized variable thrust rocket engine and ramjet propulsion.

对于泵压式变推力发动机和先进的冲压发动机,需要涡轮泵变工况工作,涡轮泵变工况性能是该类发动机研究的一个重点。

77. 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

78. Numerical simulation of effect of disturbing on starting state of ramjet engine inlet

扰动对超声速进气道起动状态影响的数值模拟

79. Demand Mode Integral Rocket Ramjet

指令型整体式火箭冲压喷气发动机

80. The water ramjet based on the reaction of water and fuel is a new kind of underwater engine.

摘要基于水与金属燃料反应的水冲压发动机是一种新型的水下动力装置。