| 1. | Of all the aerodynamic parameters required in stability and control analysis, the hinge-moment coefficients are most difficult to determine with precision .
进行稳定性和操纵性分析所需要的全部空气动力参数中，铰链力矩系数最难准确地确定。 |
| 2. | Pitching moment coefficient
俯仰力矩系数 |
| 3. | Heeling moment coefficient
倾侧力矩系数 |
| 4. | Rolling moment coefficient
滚动力矩系数 |
| 5. | Damping torque coefficient
阻尼力矩系数 |
| 6. | Finally radial basis function ( rbf ) is adopted to identify the moment coefficient
最后还采用径向基函数神经网络识别了力矩系数。 |
| 7. | With the increase of the relative velocity , the variations of side force coefficient and yawing moment coefficient of the overtaken vehicle will increase linearly
被超车侧向力系数和横摆力矩系数的变化量随两车相对车速的增加呈线性增加的趋势。 |
| 8. | The theory of complex - moment - coefficient method is provided due to ssr , and the relationship between complex - moment - coefficient d ( m ) and subsynchronous frequency is also illustrated
在ssr研究中，主要阐释了复数力矩系数法研究的机理，探讨了复力矩系数d ~ ( ( m ) )与次同步频率的关系。 |
| 9. | This paper adopts linear interpolation to deal with data of wind tunnel experiment for sample uav and realizes modeling and simulation of the sample uav with c language in common aerodynamics and moment coefficient
本文采用线性插值处理样例无人机风洞试验数据，采用正常情况下的气动力及力矩系数数学模型，并用c语言实现样例无人机建模与仿真。 |
| 10. | The aerodynamic objective function is described as some aerodynamic parameters gained by reynolds - averaged n - s equations , such as : the lift , the drag , the ratio of lift to drag or the pitching moment , etc . the optimum process is started by a base airfoil
本文采用基于n - s方程的流场计算程序来求解流场，得到升力系数、阻力系数、力矩系数等气动参数，并以其中某个或某些参数构成目标函数。 |
