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气动弹性的英文
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- 英文翻译
- 造句
- aeroelasticity
- 气动 pneumatic
- 弹性 elasticity; resilience; spri ...
- 气动弹性型 aerodynamic-elastic modes
- 气动弹性学 aeroelasticity; aeroelastics
- 气动弹性裁剪 aeroelastic tailoring
- 气动弹性导数 aeroelastic derivative
- 气动弹性发散 aeroelastic divergence
- 气动弹性理论 aeroelastic theory
- 气动弹性力学 aeroelasticity; aeroelastics
- 气动弹性模型 aeroelasticaly model
- 气动弹性扭转 aeroelastic torsion
- 气动弹性试验 aeroelastic test
- 气动弹性特性 aeroelastic characteristics
- 气动弹性效应 aeroelastic effects
- 气动弹性载荷 aeroelastic load
- 气动弹性振动 aero-elastic vibration; aeroelastic oscillations
- 热气动弹性的 thermoaeroelastic
- 气动弹性不稳定性 aeroelastic instability
- 气动弹性静力学 static aeroelasticity
- 气动弹性力学家 aeroelastician
- 气动弹性稳定性 aeroelastic stability
- 气动弹性翼理论 aeroelastic wing theory
- 热气动弹性力学 thermoaeroelasticity
- 动弹性 dynamic elasticity
- 气动弹道 aerodynamic trajectory
- The research of this dissertation is focused on how to solve the 3 - dimensional compressible navier - stokes equations by the implicit finite difference algorithm and to simulate numerically the unsteady subsonic and transonic viscous flows around rigid and elastic wings . on the base of them the aeroelastic characterictics of an elastic wing have been studied
本文的主要工作是用隐式有限差分法求解三维非定常紊流n - s方程组，数值模拟刚性机翼及弹性机翼的亚、跨、超音速定常及非定常粘性绕流，并在此基础上研究了弹性机翼的气动弹性问题。 - The conventional model construction method , rational functional approximation method , ca n ' t describe the nonlinear effect of the nonlinear unsteady aerodynamics . so the reduced order model based on volterra series for linear and nonlinear unsteady aerodynamics was investigated and applied to the model construction and active control law design of aeroelastic system
针对气动伺服弹性分析与设计中传统的有理函数拟合法不能够有效地描述非线性效应的问题，本文研究了基于volterra级数的非定常气动力降阶模型( rom )及其在气动弹性系统主动控制律设计中的应用。 - Secondly , the static aeroelastic problems and jig - shape design , as a kind of multi - disciplinary design optimization ( mdo ) , are investigated for sweep wing and super - critical wing . numerical results are in good agreement with other reference data . the method and the program presented in this paper are verified
分别以某后掠机翼和超临界机翼为算例，对机翼的静气动弹性问题以及基于静气动弹性的型架外形优化设计和飞行姿态确定进行研究，计算结果和有关文献的结果进行了比较，吻合很好。
- 气动弹性的日语：くうりきだんせい
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Last modified time:Sun, 10 Aug 2025 00:29:56 GMT
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