Computation of the Two-Dimensional Incompressible Turbulent Flow Around a Wing Section in Cascade
スポンサーリンク
概要
- 論文の詳細を見る
Computation of the two-dimensional incompressible turbulent flow around a wind section in cascade was made using the finite difference method. The computational scheme used in this paper is based on the Implicit Approximate Factorization scheme, which has been developed at the Ship Research Institute. The overlapping grid technique was used in order to generate well-conditioned, body-fitted coordinates for the complicated computational domain around a cascade wing section easily. The computed results were compared in two steps. Firstly, the comparative computational study between the present method and the higher-order boundary layer integral method was carried out and the merit and demerit of the present scheme were discussed in detail. Secondly, the comparison with experimental data (lift and drag coefficient) was made. The present method showed reasonable agreement with them.
- 独立行政法人 海上技術安全研究所の論文
- 1989-07-31