| COMPUTATION OF COMPRESSIBLE FLOW PAST SLENDER WING－BODY USING FULL－POTENTIAL EQUATION |
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| 作者姓名： | Huang Mingke |
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| 作者单位： | Department of Aerodynamics，Nanjing University of Aeronautics and Astronautics，Nanjing，China，210016 |
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| 摘 要： | ＣＯＭＰＵＴＡＴＩＯＮＯＦＣＯＭＰＲＥＳＳＩＢＬＥＦＬＯＷＰＡＳＴＳＬＥＮＤＥＲＷＩＮＧ－ＢＯＤＹＵＳＩＮＧＦＵＬＬ－ＰＯＴＥＮＴＩＡＬＥＱＵＡＴＩＯＮＨｕａｎｇＭｉｎｇｋｅ（ＤｅｐａｒｔｍｅｎｔｏｆＡｅｒｏｄｙｎａｍｉｃｓ，ＮａｎｊｉｎｇＵｎｉｖｅ...
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COMPUTATION OF COMPRESSIBLE FLOW PAST SLENDER WING-BODY USING FULL-POTENTIAL EQUATION |
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| Huang Mingke.COMPUTATION OF COMPRESSIBLE FLOW PAST SLENDER WING-BODY USING FULL-POTENTIAL EQUATION[J].Chinese Journal of Aeronautics,1996(1). |
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| Authors: | Huang Mingke |
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| Abstract: | The H-O grid is suggested to compute compressible flow past highly swept slender wing-body combinations. Full-potential equation, finite difference method and approximate factorization scheme are used. The computations for the AGARD-B wing-body show that the code developed can apply to the cases from subsonic up to low supersonic free stream. The computed lift and pitching moment are in good agreement with the experimental results. |
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| Keywords: | grids compressible flow sweepback finite difference theory subsonic flow supersonic flow |
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