搜索资源列表
boundary
- 计算气动力边界条件，非守恒无激波跨声速情况下使用
Application
- 对弹丸飞行稳定性进行了分析,文中提出利用M GAERO 气动软件计算弹丸的气动力参数,以减少采 用经验公式估算气动力系数和压心位置等参数带来的误差,可为弹丸飞行稳定性分析和总体参数设计提供 参考依据。-For projectile flight stability analysis, this paper proposes the use of software to calculate projectile M GAERO aerodynamic aerodynamic paramet
gaochao
- 空气动力学高超声速 简单飞行器 气动力计算 -Aerodynamics of hypersonic aircraft aerodynamic calculations
flutter_program_matlab
- 飞行器机翼非定常气动力计算及颤振计算程序！-Flutter calculation procedures flutter calculation procedures flutter calculation program
qidongli
- Grossman气动力，可用于获取Volterra级数一阶核的特征系统辨识的输入输出仿真。-Grossman aerodynamics can be used to obtain a first-order Volterra series features core simulation input and output system identification.
chaoyinsuyixing
- 该程序研究了攻角为2度的条件下超音速翼型的气动力特性。-This program studies the aerodynamic characteristics of of supersonic airfoils under an attack angle of 2 degrees .
Aerodynamic-calculation
- 三角形机翼，气动力，画网格，算法实例，好好参考-THE REAL EXAMPLE
Aerodynamic Force
- 飞机气动力计算的程序，根据实际参数估算不同飞行状态下的气动力系数。(The aerodynamics calculation program, used to estimate aerodynamic coefficients under different flight conditions.)
Theodorsen -vg
- 通过西奥道森气动力模型求解气动力，并通过v-g法求解颤振速度与颤振频率(Solve the aerodynamic force through the Theodorsen aerodynamic model and solve the flutter velocity and flutter frequency through the v-g method)