2025-08-15 19:52 浏览次数 8
不稳定载荷
a kernel function method and the results of computing unsteady load on three-dimensional wings in transonic flow are presented in this paper. the method is based on linearized lifting surface theory.
本文给出了在跨音速流动中,计算三维机翼非定常载荷分布的核函数法和计算结果。