标题： 可压缩粘性纳维-斯托克斯微分方程解的精确分布：航空工业中的应用 显示英文标题

标题： Exact Distributions for the Solutions of the Compressible Viscous Navier Stokes Differential Equations: An Application in the Aeronautical Industry

摘要： 风洞和线性化湍流及边界层模型到目前为止一直是通过统计确定或近似的相关情境系数值，如阻力和升力系数，来模拟和近似(底座安装的)机翼上的静止升力和阻力的必要手段。为了改进这一过程，我们引入了瞬态和精确的公式，通过求解纳维-斯托克斯微分方程流体动力学模型得到的解，提前分离这些力。 显示英文摘要

摘要： Wind tunnels and linearized turbulence and boundary-layer models have been so far necessary to simulate and approximate the stationery lift and drag forces on (base-mounted) airfoils by means of statistically determined or approximated values of the relevant situational coefficients as the drag and lift coefficients.To improve this process, we introduce transient and exact formulae to separate these forces in advance by means of the solutions found from the fluid dynamics model of the Navier Stokes differential equations.