Inverse wing design in transonic flow including viscous interaction
Inverse wing design in transonic flow including viscous interaction
复制标题
跨音速流中的逆翼设计，包括粘性相互作用
DOI：
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复制
发表时间：
1989
期刊：
影响因子：
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通讯作者：
R. L. Campbell
中科院分区：
文献类型：
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作者：
L. Carlson;R. Ratcliff;T. Gally;R. L. Campbell
几个逆方法进行了比较，初步结果表明，结果的差异主要是由于坐标系和机身表示，而不是设计程序。此外，从一个直接的反方法，包括3-D机翼边界层的影响，尾流曲率和尾流位移的结果表示。这些结果表明，边界层位移必须包括在设计过程中的准确结果。
Several inverse methods were compared and initial results indicate that differences in results are primarily due to coordinate systems and fuselage representations and not to design procedures. Further, results from a direct-inverse method that includes 3-D wing boundary layer effects, wake curvature, and wake displacement are represented. These results show that boundary layer displacements must be included in the design process for accurate results.