hypersonic

hypersonic

1. For it s excellent performance, Rocket-Based-Combined-Cycle (RBCC) should be the most competitive propulsion system of Hypersonic Flight Vehicle for martial and civil purpose.

RBCC发动机性能分析模型在高超声速飞行器方案选择、总体设计以及RBCC发动机设计与性能分析等方面具有极其重要的作用。

2. TVD scheme and numerical simulation of aerodynamic heating in hypersonic flows

TVD格式与高超音速气动加热数值模拟

3. Hypersonic inviscid flow computation over X-38 with unstructured meshes

X-38飞行器无粘绕流的非结构网格模拟

4. And over the next several decades, the scramjet work could eventually provide China with a tactical hypersonic global-strike capability beyond the country's strategic ballistic missile force.

“中国是具备在军事上和美国竞争的最有潜力的国家，假以时日，中国的区域破坏性军事技术能够抵消美国的传统军事优势。”

5. integrated hypersonic vehicle

一体化高超声速飞行器

6. To analyze radar scattering of underdense plasma turbulence of hypersonic reentry wake , fluctuation background parameters of turbulence field are needed.

为给高超声速再入尾迹亚密湍流雷达散射分析提供所需的脉动背景场参数,本文提出计算非平衡再入湍流尾迹脉动等离子体场的理论方法。

7. It has been studied for the application of genetic algorithm on the aerothermodynamics and aerodynamic optimum design of hypersonic aircraft.

主要内容有:1.把遗传算法引入到高超声速气动优化中来。

8. William H, David T, Daniel H. Hypersonic airbreathing propulsion. Washington, D. C.: American Institute of Aeronautics and Astronautics, Inc. , 1994.

乐嘉林,刘陵.高超声速飞行器的碳氢燃料双模态超燃冲压方案研究,推进技术,1998(1

9. Investigation of waverider configuration in hypersonic wind tunnel

乘波外形高超声速风洞测力试验研究

10. As a kind of new configuration waveriders have high lift to drag ratio (L/D) in hypersonic flight, which makes the study of waverider shapes an important trend of hypersonic air vehicles development.

乘波构形在高超声速条件下的高升阻比优势备受关注，使得对于它的设计研究成为高超声速飞行器外形设计的一个重要方向。

11. The unsteady aerodynamic characteristics of waverider aircraft is one of the most important physical problems in hypersonic flight.

乘波飞行器运动过程中的非定常气动特性是高超声速飞行中的重要物理问题之一。

12. A conceptual design of the hypersonic civil transport is introduced here.

介绍了高超声速民用运输机的概念设计方案。

13. FEM FCT is used to solve three dimensional hypersonic inviscid flow.

从Euler方程出发，利用流量修正有限元法（FEM?FCT）求解三维无粘流动的高速流场。

14. Atmospheric reentry generates tremendous heating on the undersurface of spacecraft (a couple of thousand degrees Celsius) caused by the friction of the air rushing by at hypersonic speeds.

以极音速重返大气时，空气造成的摩擦在太空船底部表面产生极高的热（大约为摄氏数千度）。

15. So many countries put their eyes on the Hypersonic Cruiser Vehicle which can fill current capability shortfalls in exiting weapons.

优化不仅可以节省成本而且对于在同等成本条件下某项性能达到更高的指标都有一定的指导意义。

16. Hypersonic wind tunnels operating at very low densities were developed starting in about 1960.

低密度超音速风洞大约开始发展于1960年。

17. Numerical solutions agree with supersonic linearized potential flow theory as a special case when the mean angle of attack tends to zero and with piston theory in hypersonic case.

作为平均迎角趋于零的特殊情况,本文的数值结果与超声速线化的位流理论是一致的,在高超声速情况与活塞理论一致。

18. According to the analyzing method of characteristic quantities for flows sub-processes,this paper presents a law of similitude for hypersonic chemical reaction flows.

依据流动子过程特征量分析方法，导出了高超声速化学反应流动的相似律。

19. Advanced Hypersonic Manned Aircraft

先进超音速有人驾驶飞机

20. Numerical simulation of hypersonic flow field around the reentry vehicle

再入三维高超声速粘性流场的数值模拟

21. The thermal environment and ablation characteristics of the vehicle with carbon-based material were analyzed under hypersonic conditions.

分析了高超声速情况下球双锥再入体选用碳基防热材料的热环境和烧蚀特性。

22. Transient interaction flow field of the multi-lateral jet hypersonic interceptor in the aerosphere was calculated by means of unsteady Navier-Stokes equations.

利用非定常N-S方程数值求解技术,计算了大气层内高超音速拦截弹带多个横向喷流的瞬态干扰流场,为拦截弹瞬态多侧向喷流的精确控制力建模提供了理论参考依据。

23. Lifting-body hypersonic vehicles

升力体高超声速飞行器

24. Cross-section design of a controllable hypersonic inlet. The research is being done at the Nanjing University of Aeronautics and Astronautics.

南京航空航天大学正在进行一个可控高超音速进气道断面设计研究。

25. A new method of quickly generating hypersonic waverider forebody configurations was developed.

发展了一种基于分析法的高超声速乘波构型飞行器前体设计方法。

26. inflatable hypersonic vehicle

可膨胀飞行器

27. Rotornet: A High-Performance Hypersonic Decelerator for Planetary Entry

叶轮网,进入轨道用的高性能超音速减速器

28. The core of airbreathing technology is scramjet and airframe/propulsion integrated hypersonic flight vehicle.

吸气式高超声速技术的核心是超燃冲压发动机技术和机体／推进一体化飞行器技术。

29. Conceptual Design of an Airbreathing Hypersonic Civil Transport

吸气式高超声速民用运输机概念设计

30. Air-breathing hypersonic vehicle

吸气式高超声速飞行器

31. Air-breathing hypersonic vehicle(AHV) has been the next generation single stage to orbit vehicle and hypersonic cruise vehicle.

吸气式高超声速飞行器是下一代单级入轨和高超声速巡航研究的重点飞行器。

32. With such a large heat sink value, FRA can meet the requirement of hypersonic flying machine.

在 80 0℃时 ,两者都具有较高的热沉值 ,分别达到 5 6 9MJ kg和 6 6 0MJ kg ,该热沉值能够满足超高音速飞行器的热管理要求。

33. Ames Dimensional Hypersonic Wind Tunnel

埃姆斯量纲高超音速风洞

34. Simulation of Hypersonic Non-Equilibrium Flow Using Hybrid Grids

基于混合网格上的高温非平衡流的数值模拟

35. For hypersonic vehicles,the effect of nozzle aerodynamic characteristics on vehicles performance is serious.

基于特征线法,并考虑变比热的影响,开展了高超声速飞行器用单膨胀斜面喷管设计。

36. Optimization Design of Hypersonic Inlets Using Genetic Algorithm Based on a Parabolized Navier-Stokes Flow Solver

基于遗传算法和空间推进方法的高超声速进气道优化设计研究

37. The success application of the method introduced in the paper demonstrates the practicability and responsibility of all algorithms in optimization design of hypersonic aircraft.

对已有的气动分析模块及其优化方法进行气动优化设计,来考察各种方法在高超声速优化设计中的应用情况,检验优化前后气动性能的改善程度。

38. Moreover, the characteristics of evolution for the disturbances of different modes in the hypersonic sharp cone boundary layer was discussed.

并进一步讨论了不同模态初始扰动在高超音速尖锥边界层中的演化规律。

39. The hypersonic gas flow of vertical plate is simulated by using hybrid DSMC/EPSM code and the DSMC method. Through the comparison of the results, the effectiveness of the DSMC/EPSM code is proved.

应用该算法对汲及化学反应的二维高超音速竖板绕流流场进行模拟 ,将结果与 DSMC方法的结果进行比较 ,验证了新算法对求解化学反应流动的可行性。

40. The hypersonic gas flow of flat-nosed cylinder is simulated by using hybrid DSMC/EPSM code and the DSMC method. Through the comparison of the results, the effectiveness of the DSMC/EPSM code is proved.

应用该算法对汲及化学反应的轴对称情况下高超声速平头圆柱绕流流场进行模拟,将结果与DSMC方法的结果进行比较,验证了新算法对求解化学反应流动的可行性。

41. The new algorithm is used for the tomographic reconstructions of the density distributions in rocket exhausted jet and hypersonic flow, and some errors of the reconstruction result are discussed.

应用该算法，对火箭燃气射流场和高超音速流场的莫尔偏折图进行了处理和计算，重建出流场截面的密度分布，并对重建结果进行了分析。

42. QIN N, REDLICH A.Massively separated flows due to transverse sonic jet in hypersonic laminar stream [R].AIAA 96-1934.

庞勇,贺国宏.高超声速流场中侧向喷流效应的数值模拟研究[A].第十届全国高超声速气动力(热)学术交流会论文集[C],1999:210-216.

43. THE STUDY OF AERODYNAMIC HEATING AND ABLATION FOR HYPERSONIC PROJECTILE WING

弹翼表面气动加热和烧蚀现象的研究

44. The results obtained here provide a reference for the application of detonation in the hypersonic propulsion.

当前研究为爆轰燃烧在高超声速推进中的应用提供了重要参考。

45. Keywords Extended-arc;hypersonic plasma jet;sprayed particle;ceramic coating;

扩展等离子弧;超音速等离子焰流;喷涂颗粒;陶瓷涂层;

46. It has been studied for the application of traditional optimum algorithm on the aerothermodynamics and aerodynamic optimum design of hypersonic aircraft.

把传统的优化方法引入到高超声速气动优化中。 传统的优化方法最主要的是梯度法,文中将对梯度法及其改进的变度量法进行研究,并把他们应用到高超声速优化中来。

47. In order to grasp the hypersonic vehicle models complex dynamic characteristics, a new hypersonic vehicle model method was proposed.

摘要为了掌握高超音速飞机复杂的动态特性，提出了一种研究高超音速飞机模型的新方法。

48. The SERN of a hypersonic vehicle was designed for improving the lift and propulsion force.

摘要为了提升高超声速飞行器单壁膨胀喷管的升力和推力，对其进行了优化设计。

49. To set up Multidisciplinary Design Optimization (MDO) software system of hypersonic flight vehicle, a kind of modeling method oriented to MDO was studied.

摘要为建立高超声速飞行器多学科设计优化软件系统，研究了一种面向多学科设计优化的建模方法。

50. For design of internal contraction tunnel and isolator of two-dimensional hypersonic inlet, curved surface structure at the bottom wall was presented.

摘要对于二元高超声速进气道内压缩通道及隔离段设计，提出了进气道下壁弧形曲面构型方案。

51. This paper advances a calculation model based on the computational fluid dynamics (CFD) and Fourier-optics method to study infrared light transmission in a hypersonic fluid filed.

摘要提出了一种基于CFD网格和傅里叶光学方法的高速流场中红外光传输的计算模型。

52. Using axisymmetric full Navier-Stokes equations, the thermo-chemical nonequilibrium flow in hypersonic nozzle was simulated and the scale effects due to nonequilibrium were analysed numerically.

摘要采用轴对称热化学非平衡全N-S方程，数值分析了高超声速喷管流场中非平衡引起的尺度效应。

53. A new Jacobian matrix splitting method for ideal three-dimensional MHD (magnetohydrodynamics) equations was developed and verified by numerically simulating 3D hypersonic MHD flows.

摘要针对三维理想MHD方程提出了一种新的雅可比矩阵分裂方法，并成功地应用于磁场干扰下的三维高超声速磁流场流数值模拟。

54. Hypersonic propulsion test facility is important for the scramjet ground tests.

摘要高超声速推进风洞是进行超燃冲压发动机模型地面模拟的重要试验设备。

55. A fresh method on the condition of hypersonic speed, based on disturbance observer and dynamic inversioncontrol is introduced in this paper in order to solve the stability of flight control system.

文中介绍了在高超音速条件下,基于干扰观测器和非线性动态逆控制的方法,对飞行器姿态控制系统的稳定性的研究。

56. Abstract: A numerical algorithm to simulate the hypersonic inviscid Flow fields of chemical non-equilibrium is presented in this paper .

文摘:本文给出了求解高超声速化学非平衡无粘流场的数值模拟方法。

57. Abstract: Model free flight experiments were carried out in impulse hypersonic wind tunnel at Institute of Mechanics, Chinese Academy of Sciences to obtain pitching damp of two space shuttle models.

文摘:采用模型自由飞技术在脉冲型高超声速风洞中测量了两种类航天飞机外形模型的俯仰阻尼导数。

58. A TIME magazine display at the convention will feature speeches of past Republican presidents in tightly controlled beams of HyperSonic Sound (HSS).

时代杂志展示了大会将用这种超音速声音（HSS）的紧密的控制的柱来放映前共和党总统的演讲。

59. Multidisciplinary modeling and simulation of a generic hypersonic vehicle

普通高超音速飞行器的多学科建模与模拟

60. Hypersonic pitching damp measurements for a winged vehicle by model free flight

有翼飞行器高超声速动导数的风洞自由飞测量

61. An artist's rendering depicts the takeoff of an A2 aircraft, a proposed hypersonic jet unveiled this week by British engineers.

本周要推出的由英国工程师倡议的A2型超超音速飞机，此为飞机起飞的艺术效果图。

62. The design concept and principle of injector valve system of hypersonic wind tunnel controlled by the computer are introduced in this paper.

本文介绍了高超声速风洞引射器阀门系统采用计算机控制的设计思想和原理框图。

63. The results of numerical simulation of the hypersonic flow around a plate with a sharp leading edge are presented.

本文描述绕锐前缘平板高超声速流动的数值模拟结果。

64. A simplified flow field model and simple air chemical model for the chemical nonequilibrium trailing wakes of hypersonic non-ablating blund-body are presented.

本文提出了一个高超声速非烧蚀钝体化学非平衡尾流流场的简化模型和简化的空气化学模型。

65. In this paper we develop a wedge-elliptical cone waverider configuration method, study on front body-scramjet engine integration design, and create a hypersonic waverider.

本文提出了一种变楔角楔/椭圆锥乘波体构型方法,并基于前体/进气道一体化设计思想,生成了高超声速乘波飞行器构型。

66. The experimental results of low temperature ablator (beeswax and camphor) tests in the hypersonic wind Tunnel are presented in this paper.

本文给出了低温烧蚀材料的高超声速风洞烧蚀实验研究的结果。

67. A numerical algorithm to simulate the hypersonic inviscid Flow fields of chemical non-equilibrium is presented in this paper .

本文给出了求解高超声速化学非平衡无粘流场的数值模拟方法。

68. In this paper the results of calculations of the coefficients of skin friction and heat transfer(Stanton number) on the surface of hypersonic flight vehicle are presented.

本文给出了高超声速飞行器表面摩阻和传热系数 (斯坦顿数 )的计算结果。

69. In this thesis, the aerodynamic heating methods of hypersonic projectile are presented.

本论文进行了高超声速弹丸的气动热研究。

70. On a recent project, for example, I ran my persistence unit tests inside of Eclipse using HSQL and local datasources against a Hypersonic SQL database using Hibernate Transaction manager.

比如在最近的项目中,我在Eclipse中,使用HSQL和本地数据库对使用Hibernate事务管理器的Hypersonic SQL数据库进行持久性单元测试。

71. Boeing Hypersonic Wind Tunnel

波音(公司)超高速风洞

72. Preliminary design for soaring hypersonic cruise vehicle

滑跃式高超音速巡航飞行器设计初步研究

73. And that, says Mike McKeon, PWR's manager of Hypersonic and Advanced Programs, is key.

热燃气流穿过狭窄的喉道时，再次被加速到声速，然后膨胀，冲出倒锥形的喷管，达到超声速。

74. Departures form the ideal practice followed by the Wright have been particularly noticeable in the development of supersonic and hypersonic vehicles.

特别值得注意的是在发展超音速和高超音速飞行器的过程中，偏离了莱特理想的工作方式。

75. hypersonic similarity parameter

特超声速相似参数

76. hypersonic flight aerothermodynamics

特超音速(飞行)气动热力学

77. The airframe and engine highly integration nature of hypersonic vehicle results in the asymmetry and cowl adjustable characters of the scramjet nozzle.

由于高超声速飞行器机体与发动机高度一体化的构型,使超燃冲压发动机尾喷管具有非对称,面罩可调等特点。

78. Effects of Real Gas on Aerodynamic Characteristics of a Hypersonic Orbiter

真实气体效应对高超声速轨道器气动特性的影响

79. Because of the limitation of experiment equipment, numerical methods have become the main method to research hypersonic flows.

研究高 超音速流动由于地面试验模拟条件的限制，数值模拟成为其主要的研 究手段。

80. There are a large number of aerodynamic heat, in particular during hypersonic re-entry, aerodynamic heating results in ultra-high surface temperature.

空天飞行器以高超声速返回再入大气层时，气动加热会使其表面达到极高的温度。