aeroelasticity

  • n.气动弹性;空气弹性;(航)气动力弹性学
aeroelasticityaeroelasticity
  1. Numerical Simulation of Unsteady Flow Field and Its Application to Aeroelasticity

    非定常流场数值模拟及在气动弹性中的应用

  2. Application of Regress Analysis Method to Aeroelasticity Research

    回归分析方法在气动弹性研究中的应用

  3. Design Method of Active Control Law Based on Reduced Order Model of Unsteady Aerodynamics for Aeroelasticity

    基于非定常气动力低阶模型的气动弹性主动控制律设计

  4. Airfoil flutter is one of the important problems in aeroelasticity .

    在气动弹性力学中,机翼振颤是一个非常典型的问题。

  5. Application of Galerkin Finite Element Method to Rotor Aeroelasticity

    伽辽金有限元素法对旋翼气弹稳定性的应用

  6. An Analysis of Structure Response for Transonic Static Aeroelasticity

    跨声速静气动弹性结构响应分析

  7. Study on Problems of Aeroelasticity of Box Girder for Long-Span Suspension Bridge

    大跨悬索桥箱梁气动弹性问题研究

  8. The investigation and application of the technique of CFD simulation to static aeroelasticity correction

    CFD技术在静气动弹性修正计算中的研究与应用

  9. A numerical method in aeroelasticity for wings with separation at large angle of attack

    大攻角机翼的气动弹性计算方法

  10. Then the aerodynamic force in the formula is derived by using aeroelasticity theory .

    此外,本文还基于能量守恒原理推导了附加质量和气动阻尼的解析公式,并运用气动弹性力学原理对附加质量和气动阻尼中的气动力项进行了推导。

  11. The Study of the Green 's Function Method and its Application to Aeroelasticity and Aerodynamic Load Calculations

    格林函数方法研究及其在气动弹性和气动载荷计算中的应用

  12. Then the aeroelasticity is investigated by using the Euler equations and structure equations .

    并以Euler方程为主控方程,耦合结构运动方程对二维翼型进行了颤振特性研究。

  13. The longitudinal stability of elastic vehicles is studied with the effect of aeroelasticity considered .

    本文研究考虑气动弹性时飞行器的纵向稳定性问题。

  14. NUMERICAL METHOD OF AEROELASTICITY BASED ON LOCAL PISTON THEORY Investigation of two aeroelasticity problems in transonic flow

    基于当地流活塞理论的气动弹性计算方法研究两种跨声速气动弹性问题分析研究

  15. Aeroelasticity of Long-Span Rigid Frame Bridges under Construction Stage

    大跨刚构桥梁气动弹性试验及分析

  16. Flutter is a kind of complicated aeroelasticity instability phenomenon .

    颤振是一种复杂的气动弹性不稳定现象。

  17. Aeroelasticity is the mutual interaction between aerodynamics and a flexible body .

    柔性体和气动力之间的相互作用导致飞行器气动弹性问题。

  18. Realizing data exchange to reflect coupling between fluid and structures is essential to solving static aeroelasticity problems .

    研究静气动弹性问题一大关键是要解决流固数据耦合。

  19. Review of Experimental Research on Aeroelasticity of Turbomachinery

    叶轮机气动弹性力学实验研究回顾

  20. The Numerical Simulation of Internal Flow and Blade Aeroelasticity of Axial-fans in Beijing Subway

    北京地铁轴流风机内流场及叶片气动弹性的数值模拟研究

  21. This paper took modeling as the main research content , and analyzed / restrained the phenomena of aeroelasticity based on the model .

    本文以近空间大展弦比无人机的气动弹性建模为主要研究内容,并基于模型对气动弹性现象进行分析和抑制。

  22. Coupled with the structural equations , the models for transonic aeroelasticity in state - space are got .

    耦合结构动力学方程,建立了基于状态空间的跨声速气动弹性分析模型。

  23. Computational aeroelasticity with an unstructured grid method

    基于非结构网格的气动弹性数值方法研究

  24. The aeroelasticity analysis for turbomachinery is necessary .

    叶轮机械的气动弹性问题是流固耦合的一个重要分支,对其进行气动弹性分析是非常必要的。

  25. There are many new problems of aeroelasticity which are introduced by the novel concepts and system characteristics in the design process of hypersonic vehicles .

    高超声速飞行器设计上的特点带来了一系列的气动弹性新问题。

  26. To explore the problem of aeroelasticity of flexible wing , the engineering aeroelastic modeling and structural dynamics analysis method were studied .

    针对大展弦比机翼气动弹性问题,进行气动弹性工程化建模和结构动力学分析。

  27. In this thesis , a study of strength and aeroelasticity analysis for wings of an unmanned aerial vehicle is presented .

    本文主要对无人机机翼的结构强度及气动弹性进行分析。

  28. Aircraft servo - aeroelasticity stability

    飞机的伺服-气动弹性稳定性

  29. There are many complex unsteady flow problems including moving boundary , such as aeroelasticity , fluid-structure coupling , multi-body separation problems .

    在实际工程应用当中,经常会遇到带有移动边界的复杂的非稳态流动问题,例如空气弹性变形,流固耦合问题,多体分离问题等。

  30. Utilizing the plunging and pitching signals as the feedback , the principle of active aeroelasticity is studied in detail .

    即利用二元机翼的沉浮、俯仰运动的位移、速度信号作为反馈控制信号,对主动气动弹性系统进行原理性研究。