Method for expanding volume of wave rider by using cubic polynomial
A polynomial and waverider technology, applied in the field of hypersonic aerodynamic design, can solve problems such as small volume, adverse effects of inlet installation, increased resistance, etc., and achieve the effect of reducing the impact of waveriding performance
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[0025] The lower surface is the waverider surface obtained by streamline tracing in the shock flow field.
[0026] Use cubic polynomials to construct the upper surface to increase the volume, modeling schematics and coordinate systems such as figure 1 As shown (half model), the apex of the waverider is the origin of the coordinates, and the coordinates in the longitudinal direction, spanwise direction and height direction are represented by x, y and z respectively.
[0027] First determine the leading edge curve (Leading Edge), the leading edge curve is also the edge line of the lower surface, composed of discrete points, this three-dimensional leading edge curve can be used with the function Fit spanwise and heightwise position representations separately.
[0028] Secondly, construct the upper surface keel line (Keel Line), that is, the longitudinal section at the central symmetrical plane. As shown, using the cubic polynomial k(x)=a 0 +b 0 x+c 0 x 2 +d 0 x 3 Express...
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