| 流面坐标系特征线法对超音速三维机翼及细腰体绕流的计算 |
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| 引用本文： | 王宝舆.流面坐标系特征线法对超音速三维机翼及细腰体绕流的计算[J].航空学报,1985,6(4):393-396. |
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| 作者姓名： | 王宝舆 |
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| 作者单位： | 北京航空学院 |
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| 摘 要： | 本文根据文献〔1〕求得的流面坐标系中准确的沿两个流面（ξ3和ξ2=C2）四条双特征线法对圆-椭圆三角翼作了计算,并与文献〔2～4〕的结果作了比较。以类似方法对超音速绕细腰体的流动也作了计算并与文献〔6〕作了比较。
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| 收稿时间： | 1984-06-25; |
CALCULATION OF SUPERSONIC FLOWS AROUND A THREE-DIMENSIONAL WING AND A WAISTED BODY WITH CHARA- CTERISTIC METHOD IN STREAM SURFACE COORDINATES |
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| Wang Baoyu.CALCULATION OF SUPERSONIC FLOWS AROUND A THREE-DIMENSIONAL WING AND A WAISTED BODY WITH CHARA- CTERISTIC METHOD IN STREAM SURFACE COORDINATES[J].Acta Aeronautica et Astronautica Sinica,1985,6(4):393-396. |
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| Authors: | Wang Baoyu |
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| Institution: | Beijing Institute of Aeronautics and Astronautics |
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| Abstract: | According to the exact characteristic surface equation of three dimensions and the physical relations along bicharacteristics in stream surface coordinates of Ref. 1 , the pressure distributions of circula-elliptic delta wing and waisted body are calculated with "real" characteristic method. The results are compared with those of Refereces 2,3,4 and 6. |
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