aeroelastic

aeroelastic

1. Optimization design for aeroelastic dynamics of T-tail

T型尾翼动气动弹性优化设计

2. Ye Z Y,Wang G,Yang Y N,et al.A Method to simulate the aeroelastic problem based on Navier-Stokes equations[J],Chinese Journal of Computational Physics,2001,18(5):397-401.(in Chinese).

[1]叶正寅,王刚,杨永年,等.利用N-S方程模拟机翼气动弹性的一种计算方法[J].计算物理,2001,18(5):397-401.

3. Wan Z Q,Tang C H,Zou C Q.Static aeroelastic characteristics analysis of a flexible forward-swept composite aircraft [J].Acta Materiae Compositae Sinica,2002,19(5):118-124.

[2]万志强,唐长红,邹丛青.柔性复合材料前掠翼飞机静气动弹性分析[J].复合材料学报,2002,19(5):118-124.

4. CONSISTENCE ANALYSIS AND VALIDATION OF THREE METHODS FOR STATIC AEROELASTIC DIVERGENCE

三种静气动弹性发散方法的一致性分析和验证

5. WIND TUNNEL AEROELASTIC MODELLING OF THE CHINESE CENTRALTVTOWER

中央电视塔气动弹性风洞模拟试验

6. WIND TUNNEL STUDIES ON THE BEHAVIOUR OF AEROELASTIC TWIN CABLE MODEL

串列双索气弹模型的风洞试验研究

7. This model is specially developed for Electrical Controlled Rotor aeroelastic analysis, and can take account of the unsteady effect of flap nose overhang.

为满足电控旋翼的气弹分析需要,给出了带襟翼翼型的综合时域非定常气动力模型,该模型可以计及襟翼移轴补偿的影响。

8. Analysis of Active Aeroelastic Wing Technology

主动气动弹性机翼技术分析

9. INVESTIGATION ON ACTIVE FLUTTER SUPPRESSION AND GUST ALLEVIATION FOR AN ACTIVE AEROELASTIC WING

主动气动弹性机翼的颤振主动抑制与阵风减缓研究

10. Active Aeroelastic Wing

主动气动弹性翼

11. Nonlinear Aeroelastic Analysis of Complete Aircraft in Subsonic Flow.

亚音速流中全飞机的非线性气动弹性力学分析。

12. Modal analysis method of aeroelastic full model of cable-supported bridges is introduced.

介绍了超大跨径缆索承重桥梁极限承载力分析的现状和发展趋势。

13. A refined aeroelastic model of a helicopter rotor blade with swept tips is established based on model matching.

以动力学模型和气动模型相匹配为原则，建立了后掠桨尖旋翼的细致气弹模型。

14. A comprehensive rotor finite element aeroelastic code based on LORA01 is used to analyze the electrical controlled rotor (ECR), or is called swashplateless rotor.

以有限元旋翼气弹分析程序LORA01为基础,建立了电控旋翼的气弹分析模型,给出了一种有效的旋翼/襟翼耦合配平方法。

15. Tiltrotor's coupling of its wing, pylon and rotor is more complicated than helicopter's coupling, and the aeroelastic analysis and stability of tiltrotor appears very important.

但倾转旋翼机的机翼、短舱、旋翼间的耦合效应较一般直升机复杂,其气动弹性及稳定性问题的研究也显得更为重要。

16. Wind tunnel test on an aeroelastic model of grandstand cantilevered roof of large stadium and features of wind-induced response

体育场主看台弧形挑篷气弹模型风洞试验和响应特性

17. Review of Aeroelastic Stability Investigations for Tiltrotor Aircraft

倾转旋翼机气动弹性稳定性研究进展

18. full -scale aeroelastic mode of bridge

全桥气弹模型

19. Keywords: directional stiffness, aeroelastic tailoring, analytical approach, sensitivity,

关键词:方向性刚度,气动弹性剪裁,解析法,敏度

20. Aeroelastic Analysis of a Two-Dimensional Airfoil with Control Surface Freeplay Nonlinearity

具有操纵面间隙非线性二维翼段的气动弹性分析

21. The different influences of temperature to two aeroelastic systems are analyzed.

分析了温度对这两种热结构气动弹性系统的不同影响。

22. A METHOD TO SIMULATE THE AEROELASTIC PROBLEM BASED ON NAVIER-STOKES EQUATIONS

利用N-S方程模拟机翼气动弹性的一种计算方法

23. It is shown that COMPASS is not only an engineering optimum design software hut also an aeroelastic tailoring tool for composite aircraft wing.

利用复合材料各向异性特性和优化设计技术,开展结构气动弹性剪裁研究,是防止前掠翼发散的有效手段。

24. dynamic aeroelastic

动气弹

25. Wind tunnel test and theoretical analysis on aeroelastic model of single-rod transmission tower

单杆输电塔气弹模型风洞试验研究和理论分析

26. In addition, the mathematical model of this aeroelastic system is estabi-shed by these test results using the combined classical fitting method and DFP method.

另外根据实测数据,采用经典的拟合方法与DFP法相结合的方法,建立了气动弹性系统的数学模型。

27. therefore, designers and researchers must place heavy reliance on wind tunnel testing of aeroelastic models.

因而设计者和研究者必须高度依赖气动弹性模型风洞试验。

28. An Aeroelastic Analysis Method of Wings Based on Euler Equations

基于欧拉方程的一种机翼气动弹性计算方法

29. Aircraft Static Aeroelastic Response Analysis Based on Nonlinear Experimental Aerodynamic Data

基于非线性试验气动力的飞机静气动弹性响应分析

30. Effects of Wall Admittance Changes on Aeroelastic Stability of Turbomachines.

壁导纳变化对涡轮机气动弹性力学稳定性的影响。

31. Aeroelastic Analysis and Optimization of High-aspect-ratio Composite Forward-swept Wings

大展弦比复合材料前掠翼气动弹性分析与优化

32. AEROELASTIC OPTIMIZATION OF A HIGH-ASPECT-RATIO COMPOSITE WING

大展弦比复合材料机翼气动弹性优化

33. Structural Modeling and Aeroelastic Analysis of High-Aspect-Ratio Composite Wings

大展弦比复合材料机翼结构建模与气动弹性分析(英文)

34. Study of aeroelastic tailoring of high-aspect-ratio flexible composite wing

大展弦比柔性复合材料机翼的气动弹性剪裁

35. Similarity criterion for aeroelastic model wind tunnel test of large span roofs

大跨度屋盖气弹模型风洞试验需要满足的相似条件

36. Keywords Long-span flat roof structures;Rigid model;Aeroelastic model;Wind tunnel test;Finite element;Spectral analysis;Analysis in time domain;Wind-induced dynamic response;Wind load factor;

大跨度平屋面结构;刚性模型;气动弹性模型;风洞试验;有限元;模态分析法;时程分析法;风振响应;风振系数;

37. Correction for Damping Ratio of Wind-induced Dynamic Responses for Structural Aeroelastic Model

大跨度结构气弹模型风振响应的阻尼修正系数

38. Multiparameter comparison wind tunnel tests were conducted to study wind-induced response characteristics for long-span flat roof structure aeroelastic models.

对大跨度平屋面气弹模型的风致响应特性进行了多参数对比的风洞试验研究。

39. Pneumatic stiffness simulation of wind tunnel aeroelastic model tests for closed long-span roof

封闭式大跨屋盖气弹模型风洞试验的气承刚度模拟

40. The correction techniques of aerodynamic forces were introduced in the computation and analysis of static aeroelastic divergence.

将气动力修正技术应用于静气动弹性发散计算与分析中。

41. Effectively Analyzing Aeroelastic Model Empirical Design for Empennage Non-Lift Type Buffeting and Its Wind Tunnel Test Data

尾翼气动弹性抖振模型设计与抖振试验研究

42. Composite Rotor Blade Design Optimization for Vibration Reduction with Aeroelastic Constraints

带气弹稳定性约束的复合材料浆叶减振优化设计

43. The equations of motion with periodic coefficients for rotor/tower system are derived,and the method for analyzing the aeroelastic stability is developed.

建立了大型水平轴风轮转子／塔架耦合系统的气动弹性模型，推导了转子／塔架耦合系统周期系数运动方程，给出了气动弹性稳定性分析方法。

44. Aeroelastic Stability Analysis for Bearingless Tail Rotor in Hovering

悬停状态下无轴承尾桨气弹稳定性分析

45. High-fidelity analysis tool of both aerodynamics and structures were permitted to carry out aeroelastic analysis on these sample design scenarios.

探索了在运输机初步设计阶段的一种计及气动弹性的机翼气动/结构综合优化设计方法。

46. The aeroelastic property of a wing can he improved by using the bending-twisting coupling effect of composite material skin.

摘要利用复合材料蒙皮结构的弯扭耦合效应可以改善翼面的气动弹性特性。

47. With the broad usage of composite in newly aviation structure, the engineering aeroelastic modeling and analysis of composite wing are important project to aircraft design.

摘要新一代航空结构广泛采用复合材料，对复合材料机翼的气动弹性工程化建模和分析是飞机设计的重要任务。

48. The complicated configuration of suspension bridge with the truss stiffened girder is difficult to imitate in the wind tunnel tests of full-scale aeroelastic model of bridge.

摘要针对大跨度桁架悬索桥全桥气弹模型风洞试验问题，提出了一种新的模型设计方法。

49. Aeroelastic phenomena are significant for high-altitude long-endurance aircrafts for the large aspect ratio wing.

摘要高空长航时飞机普遍具有大展弦比机翼，其气动弹性问题尤为突出。

50. Numerical simulations demonstrate that the multi body analytical model can analyze the aeroelastic stability of the tiltrotor aircraft in the helicopter mode.

数值计算表明：建立的多体动力学模型能够快速分析直升机模式下倾转旋翼机复杂的旋翼／机翼气弹耦合动力学特性。

51. Abstract: An analytical approach is proposed to obtain the sensitivity of structural responses in aeroelastic tailoring.

文摘:进行了一种用解析方法求气动弹性剪裁中的结构响应值敏度的研究。

52. Abstract: The aeroelastic analysis of a helicopter rotor blade with the controlled oscillating trailing edge flap is presented by building an aeroelastic model of the new concept rotor blade.

文摘:通过建立带受控振荡附翼的新概念旋翼气动弹性分析模型，研究了采用受控振荡附翼的直升机旋翼气动弹性特性及其在降低旋翼振动载荷方面的有效性。

53. Mathematical model and formulations of a new tilt-rotor aircraft for aeroelastic stability analysis

新型倾转旋翼机气动弹性稳定性分析模型

54. The aeroelastic stability of bearingless tail rotor is complex, while there is no research work in this region in ou r country at present.

新型尾桨型式无轴承尾桨的气弹稳定性分析非常复杂,而目前国内在这方面的研究还是空白。

55. Also,spin rate coupling with structural damping ratio and other structural parameters have a significant influence in aeroelastic dynamic instability for spinning rocket.

旋转速率与结构阻尼及其他结构参数对气动弹性动态稳定性影响也比较显著。

56. Finally for all the above aeroelastic problems, distributed parallel computation is accomplished.

最后对以上气动弹性问题的数值计算进行了基于微机网络的分布式并行计算研究。

57. The purpose of this paper is to provide a composite aeroelastic tailoring result in a real combat wing with composite skin and metal structure inside.

本文对以象皮为复合材料层板，内部构件为金属材料的小展弦比歼击 机的机翼结构进行了气动弹性剪裁。

58. The analysis method proposed in the paper can be applied to the flutter stability analysis for a multi-DOF aeroelastic system with time-delayed feedback control.

本文建立的分析方法可推广应用于带延迟反馈控制的多自由度气动弹性系统的颤振稳定性分析。

59. AEROELASTIC ANALYSIS OF AN AIRFOIL'S STALL FLUTTER AT LARGE MEAN INCIDENCE ANGLE

机翼大攻角下失速颤振的气动弹性研究

60. The aeroelastic phenomena which result may be subdivided under the heading static and dynamic.

柔和造成的气动弹性现象可以再分为静态和动态两个专题。

61. STATIC AEROELASTIC CHARACTERISTICS ANALYSIS OF A FLEXIBLE FORWARD-SWEPT COMPOSITE AIRCRAFT

柔性复合材料前掠翼飞机静气动弹性分析

62. According to the experience and the result calculated in this paper, the structure which satisfy the strength requirement usually could not satisfy the aeroelastic requirement.

根据以往的经验和本文 的计算结果。满足强度要求的飞机机翼结构，并不一定能够满足气动 弹性要求。

63. According to the dynamic analysis of the responsive skirt-air cushion system, the flexible skirt of the hovercraft can be simplified to a aeroelastic and hydroelastic dynamic feedback system.

根据响应围裙-气垫系统的动力学分析，气垫船柔性围裙可简化为一个气弹和水弹动力反馈系统。

64. As an important component of the aeroelastic model of full cable-stayed bridge, there are four laws of stiffness similarity for tower.

桥塔是全桥气动弹性模型中的重要构件,其刚度模拟应满足四个相似条件,但实际制作时,芯梁通常选用矩形断面,忽略了拉伸刚度和扭转刚度。

65. The Similarity Rules of Aeroelastic Model of High Pier Wind Tunnel Tests

桥梁高墩气动弹性模型风洞试验的相似律

66. Analytical model of aeroelastic stability of hingeless rotor blade with composite flexures

桨根柔性无铰旋翼桨叶气弹稳定性建模分析

67. aeroelastic distribution

气动力弹性分布

68. aeroelastic distortion

气动力弹性变形

69. aeroelastic interaction

气动力弹性干扰

70. aeroelastic optimization

气动弹性优化

71. aeroelastic analysis

气动弹性分析

72. aeroelastic modeling

气动弹性建模

73. aeroelastic vibration

气动弹性振动

74. aeroelastic model test

气动弹性模型试验

75. The aeroelastic phenomena may be subdivided under the heading static and dynamic.

气动弹性现象可以再分为静态和动态两个专题。

76. Overview of Flight Test Technology for Aeroelastic Critical Boundary Prediction

气动弹性稳定边界的飞行试验预测方法综述

77. aeroelastic system

气动弹性系统

78. aeroelastic problem

气动弹性问题

79. The aeroelastic problem is as old as aircraft.

气动弹性问题伴随着飞机发展的全过程。

80. aeroelastic flight test

气动弹性飞行试验