| HIGH SPEED FLOW DESIGN
USING THE THEORY OF
OSCULATING CONES AND AXISYMMETRIC FLOWS |
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| 作者姓名： | 航空学报 |
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| 作者单位： | 钱翼稷 |
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| 摘 要： | Ｃｏｎｆｉｇｕｒａｔｉｏｎａｅｒｏｄｙｎａｍｉｃｄｅｓｉｇｎｃｏｎｃｅｐｔｓａｒｅａｉｍｅｄａｔｔｈｅｄｅｆｉｎｉｔｉｏｎｏｆｆｉｎｄｉｎｇａｉｒｆｒａｍｅａｎｄｐｒｏｐｕｌｓｉｏｎｃｏｍｐｏｎｅｎｔｇｅｏｍｅｔｒｉｅｓｗｉｔｈａｃｏｎｔｒｏｌｅｄｆ...
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| H. Sobieczky.HIGH SPEED FLOW DESIGN
USING THE THEORY OF
OSCULATING CONES AND AXISYMMETRIC FLOWS[J].Chinese Journal of Aeronautics,1999,12(1):1-963. |
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| Authors: | H Sobieczky |
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| Institution: | H. Sobieczky1, |
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| Abstract: | An inverse method of characteristics was introduced into the design concept of using osculating cones (OC) in the supersonic flow, which can extend the domain of options for generating the aerospace vehicle configurations with supersonic leading edge as well as inlet diffusers. Some more practical waverider shapes with higher volumetric efficiency can be obtained through using the concept of osculating axisymmetric (OA) flows with rotationality in the post shock flow field by inputting curved shocks. |
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| Keywords: | supersonic design waveriders inlets inverse design rotational flow method of characteristics |
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