Double-cone fairing shape line optimization design method based on von Karman shape line
An optimized design and fairing technology, applied in design optimization/simulation, special data processing applications, geometric CAD, etc., can solve the problems of poor aerodynamic characteristics, complex structure, and poor manufacturability of biconical lines, and achieve superior aerodynamic characteristics, The processing technology is simple and the effect of making up for the poor aerodynamic characteristics
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[0037] Such as figure 1 As shown, the present embodiment 1 provides a method for optimal design of double-cone fairing shape lines based on von Karman shape lines, and the specific method steps are as follows:
[0038] S1 constructs the segmental equation of the fairing line based on the pre-defined characteristic parameters of the double cone fairing;
[0039] S2 Determine the deviation value between the two profile lines based on the segmental equation of the fairing profile line and the von Karman profile line equation established according to the known structural parameters of the double cone fairing;
[0040] S3 takes the minimization of the profile deviation as the optimization goal, and calculates the parameter values of the profile of the double-cone fairing;
[0041] S4 draws a biconical fairing profile line based on the parameter values.
[0042] The double cone fairing in step S1 is made up of cone top and double cone section;
[0043] The characteristic parame...
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