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- W2366164350 abstract "In order to design a novel hypersonic cruise vehicle,the test vehicle of HIFiRE Flight 1 was modified to achieve better aerodynamic performance numerically.The obtained results show that the upper surface and airfoil greatly affect aerodynamic performance of the vehicle.The lift-to-drag ratio increases continuously with the decrease of the area of the upper surface.Furthermore,without the airfoil,the lift-to-drag ratio increases with the increase of the Mach number.The wing with the waverider characteristics provides a larger lift-to-drag ratio.With the increase of the Mach number,the lift-to-drag ratio of Model 3 first increases,and then decreases.When the Mach number is 8,the lift-to-drag ratio is the largest." @default.
- W2366164350 created "2016-06-24" @default.
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- W2366164350 date "2012-01-01" @default.
- W2366164350 modified "2023-09-24" @default.
- W2366164350 title "The Design of Aerodynamic Configuration for a Novel Hypersonic Vehicle" @default.
- W2366164350 hasPublicationYear "2012" @default.
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