Optimization method for processing multiple extreme values and multiple restricted problems in flight vehicle design
An optimization method and constrained optimization technology, applied in the direction of electrical digital data processing, special data processing applications, instruments, etc., to achieve the effect of avoiding duplication of labor, ensuring feasibility, and increasing universality
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Embodiment 1
[0050] Embodiment 1: wing airfoil design optimization.
[0051] The optimization of airfoil design is of great significance to improve the overall aerodynamic performance of the aircraft. With the development of computer technology, Computational Fluid Dynamics (CFD) technology is widely used in airfoil design optimization. Taking NACA0012 as the benchmark airfoil, the CST method is used to describe the airfoil curve. The design goal is to maximize the lift-to-drag ratio of the airfoil under the premise of satisfying the constraint conditions by modifying the shape of the airfoil curve. The constraints used include: the maximum thickness of the airfoil t * max Not less than the maximum thickness t of the initial airfoil 0 max 80% of that to ensure structural strength; the lift coefficient Cl is not less than the initial airfoil lift coefficient Cl 0 To ensure that the airfoil can provide enough lift for the aircraft. The mathematical description of the problem is as foll...
Embodiment 2
[0075] Embodiment 2: Optimal design of solid rocket motor housing.
[0076]The solid rocket motor shell is an important part of the solid rocket motor, and it is an important guarantee to ensure the static strength of the engine structure and the pressure bearing capacity of the combustion chamber. Solid rocket motors are mostly disposable consumables. Under the premise of satisfying the constraints, it is hoped that its total cost will be the smallest, including the cost of materials, forming and welding. The total cost of solid rocket motor case design can be expressed as
[0077] f ( x ) = 0.622 4 x 1 x 3 x 4 + 1.778 1 x 2 x 3 2 ...
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