細長物体まわりの極超音速ソース・フロー
1980 年 28 巻 317 号 p. 277-285
詳細
1980 年 28 巻 317 号 p. 277-285
The quasi-similarity method is applied to the inviscid steady hypersonic source flow past slender bodies. Next, the results are corrected by taking into account the displacement effect of the boundary layer along the body surface, using the local similarity method. The corrected distributions of the pressure along slender powerlaw bodies of revolution are calculated, which give essentially good agreements with experimental results.
