非定常力,unsteady force
1)unsteady force非定常力
1.Both panel method and lifting surface method can be used to calculate theunsteady force.螺旋桨离散谱噪声计算一般是在螺旋桨非定常力计算和声学计算相结合的基础上得到的。
2)unsteady drag非定常阻力
3)unsteady thermal stress非定常热应力
4)unsteady aerodynamics非定常气动力
1.Volterra-series-based reduced-order model forunsteady aerodynamics;基于Volterra级数的非定常气动力降阶模型
2.Volterra series based transonicunsteady aerodynamics modeling;基于Volterra级数的跨音速非定常气动力建模
3.Fuzzy logic modeling of nonlinearunsteady aerodynamics;非线性非定常气动力的模糊逻辑建模方法
英文短句/例句
1.The Unsteady Aerodynamic Characteristics of a Wing Above Sea-Waves;风浪扰动中机翼的非定常气动力特性
2.UNSTEADY AERODYNAMIC MODELING AND IDENTIFICATION OF AIRPLANE AT HIGH ANGLES OF ATTACK飞机大攻角非定常气动力建模与辨识
3.Unsteady Flow Calculate on Using Cartesian Grid基于笛卡尔网格的非定常气动力计算
4.Reduced Order Model for Unsteady Aerodynamics and Its Application;非定常气动力降阶模型及其应用研究
5.Unsteady Aerodynamics and Aeroelastic Analysis Based on Volterra-Series;基于Volterra级数的非定常气动力和气动弹性分析
6.Stability Simulation of Unsteady Aerodynamic Based on Large-amplitude Motion;基于大振幅运动非定常气动力的稳定性仿真
7.Impact Analysis of Unsteady Aerodynamic Force on Flight Dynamics Characteristics非定常气动力对飞行动力学特性影响分析
8.CVR METHOD FOR IDENTIFICATION OF NONSTEADY AERODYNAMIC MODEL识别非定常气动力模型的初脉冲耦合振动法
9.Transonic Unsteady Aerodynamics and Flutter Computations for Complex Assemblies;复杂组合体跨音速非定常气动力和颤振计算
10.Aerodynamic Computation of 3-D Unsteady Euler Equations for Wings with Control Surface;三维带操纵面机翼Euler方程非定常气动力计算
parative Evaluation of Unsteady Aerodynamic Mathematic Models of Aircraft飞行器非定常气动力数学模型的对比分析
12.Study on Unsteady Aerodynamic Force of Morphing Joukowski Airfoil可变形儒可夫斯基翼型非定常气动力的研究
posing and adding effect of rotor blade unsteady aerodynamic force转子叶片表面非定常气动力的构成及叠加分析
14.Unsteady Transonic Flow Computation for a Wing with Control Surface Deflections by Euler Equations跨声速机翼操纵面非定常气动力Euler方程计算
15.Numerical Simulation of Aeroelasticity Basing on Indentification Technology of Unsteady Aerodynamic Loads基于非定常气动力辨识技术的气动弹性数值模拟
16.State Space Model of Unsteady Aerodynamics and Its Applicationto Aero-servo-elasticity非定常气动力状态空间模型及其在气动伺服弹性建模中的应用
17.THE AFFECTION OF INTERBLADE PHASE AnGLE IN OSCILLATING CASCADE ON UNSTEADY AERODYNAMIC FORCE振动叶栅叶片间振动相位差对非定常气动力的影响
18.Stability and Coupling Characteristics of Elastic Vehicle Acting with Unsteady Aerodynamic Forces非定常气动力作用下弹性飞行器的稳定性及耦合特性
相关短句/例句
unsteady drag非定常阻力
3)unsteady thermal stress非定常热应力
4)unsteady aerodynamics非定常气动力
1.Volterra-series-based reduced-order model forunsteady aerodynamics;基于Volterra级数的非定常气动力降阶模型
2.Volterra series based transonicunsteady aerodynamics modeling;基于Volterra级数的跨音速非定常气动力建模
3.Fuzzy logic modeling of nonlinearunsteady aerodynamics;非线性非定常气动力的模糊逻辑建模方法
5)unsteady aerodynamics非定常空气动力
1.According to the wind tunnel test data of the large-amplitude motion,the algorithm to solve fuzzy-logic model using inunsteady aerodynamics model in the recent years was modified,to increase the speed of modeling and the precision fo the model.以模型大振幅运动风洞试验数据为依据,对近几年来非定常空气动力建模中常用的模糊逻辑建模方法进行改进,使得建模速度更快、模型精度更高。
6)unsteady aerodynamic非定常气动力
1.The special additiveunsteady aerodynamic using in T-tail flutter is investig.重点研究了T型尾翼颤振计算中特殊的附加非定常气动力,建立了T型尾翼非定常气动力和颤振分析方法。
2.<Abstrcat>In order to satisfy the calculation need of Electrical Controlled Rotor(ECR, or so-called swashplateless rotor), a syntheticunsteady aerodynamic model in time domain is presented to predict the aerodynamic force and moment of the airfoil with a trailing-edge flap.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。
3.Based on the nature vibrational characteristics of the flat wing calculated by finite element method, generalizedunsteady aerodynamic forces matrix induced by the wing deformation is gotten by using strip theory, and thus the flutter model equation of the single wing is given.文中提出了一种分析亚音速下弹翼颤振临界速度的工程计算方法,其中弹翼的固有振动特性用有限元方法计算,利用片条理论计算弹翼变形诱导的广义非定常气动力矩阵,从而得到单独翼的颤振模型方程。
延伸阅读
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