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- W2385631935 abstract "The leading edge to be blunted is an efficient way to improve the aerothermodynamics performance of a hypersonic waverider vehicle.Tincher method and Takashima method are improved according to design features of waverider configuration.The CFD is used to analyze the influence of blunt leading edge on the performance of waverider.The relations of aerodynamic and aerothermodynamic characteristics to blunt radius are obtained for both blunted methods.The results show that the lift-to-drag ratios of waveriders blunted by the improved Tincher method are larger than that of waverider blunted by the improved Takashima method under the same blunt radius,the total surface areas of blunted waveriders are smaller,and the max heat fluxes are almost the same,while the heat fluxes on the leading edge except for the stagnation point are higher.So a conclusion can be drawn that the aerodynamic performances of waveriders blunted by the improved Tincher method are better than that of waveriders blunted by the improved Takashima method,but the aerothermodynamic performances are reverse.It is found that performances of waveriders are affected not only by blunt radius,but also by the blunted method.In the aerodynamic shape design of hypersonic vehicle,it is very important to choose an appropriate scheme to blunt the waverider.The results can be used for the configuration design of hypersonic vehicle." @default.
- W2385631935 created "2016-06-24" @default.
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- W2385631935 date "2011-01-01" @default.
- W2385631935 modified "2023-09-24" @default.
- W2385631935 title "Blunted Method for Waverider and Its Effect on Performance" @default.
- W2385631935 hasPublicationYear "2011" @default.
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