Chinese translation for "aerodynamic coefficient"
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- 空气动力系数
气体动力系数
Related Translations:
- Example Sentences:
| 1. | These effects appear to be negligible with respect to aerodynamic coefficients .
就空气动力系数这方面来说，这些影响似乎可以略去。 | | 2. | Effect of attack angle messurement error on extracting aerodynamic coefficients
攻角误差对拟合气动系数的影响 | | 3. | Based on in - depth survey of mess references , this thesis firstly gives comprehensive overview of aerodynamic coefficient modeling and corresponding parameter estimation algorithm
首先,本文在查阅大量近年国内外相关文献的基础上,对飞行器气动力系数建模理论及相应参数估计算法进行了综述。 | | 4. | Moreover , in order to capture the linear properties in aerodynamic coefficients , additional linear terms are added to the model , which make the wavelet network model has some definite physical significance in use
另外,本文在小波网络模型中加入状态变量的线性项,以反映气动力系数中的线性特性,这对于实际应用是非常有意义的。 | | 5. | In the paper , the computational results of all models are obtained , including 3 - d velocity field , 3 - d pressure field , and six aerodynamic coefficients . the results have good agreement with wind tunnel test
文中得出了客车外围流场的速度矢量图和压力分布图以及六个气动力系数，并将最终结果与风洞试验结果进行了比较，结果吻合较好。 | | 6. | Aerodynamic coefficient identification is a interdisciplinary subject between mechanics , informatics and control theory . this thesis also gives an overview of the development direction in this field , especially introducing the application of neural network in the aerodynamic coefficients identification , which gives the theoretical basis of using wavelet network in modeling of aerodynamic coefficients
气动系数辨识为介于力学、信息学和控制论之间的一门交叉学科,本文对该领域的发展方向进行了分析,其中特别分析了神经网络在气动力系数建模中的应用状况,这为本文采用小波网络气动系数建模打下理论基础。 | | 7. | A kind of grid generation method based on two - dimension poisson equtions is devlop - ed into the grid generation method based on three - dimension poisson equtions in this dessertation . use this method , this paper generals the grids of glide bullet to increase range that is at three states , that is with no control rudder and no tail wing , only with tail wing and with control rudder and tail wing . this paper has calculated the aerodynamic coefficients of glide bullet to increase range that is at three states . beside this the paper has given the results and analysised the differences of the three states , and the effects of control rudder and tail wing to the lift and drag . this can give us some information about the ability of the control ruder and tail wing for increasing the range
本文在二维泊松方程网格生成方法的基础上推导出了一种三维泊松方程网格生成方法。并利用该方法生成了绕弹体、尾翼弹、滑翔增程弹三种不同弹形的流场网格。计算了超音速来流下弹体、尾翼弹，滑翔增程弹三种不同弹形的空气动力学系数，分析了三种不同弹形计算结果的差别；分析了控制舵和尾翼对升力和阻力的影响。 |
- Similar Words：
- "aerodynamic chatacteristics of rotor" Chinese translation, "aerodynamic choking" Chinese translation, "aerodynamic chord" Chinese translation, "aerodynamic chord of airfoil" Chinese translation, "aerodynamic cleanness" Chinese translation, "aerodynamic coefficients" Chinese translation, "aerodynamic combustion" Chinese translation, "aerodynamic compensation" Chinese translation, "aerodynamic compressor" Chinese translation, "aerodynamic cone" Chinese translation
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