Efficient approximate optimization method for aircraft driven by heterogenous data
A data-driven, optimization method technology, applied in design optimization/simulation, special data processing applications, constraint-based CAD, etc., to reduce R&D costs, improve system performance, and improve solution efficiency and robustness.
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[0092] In order to further illustrate the purpose and advantages of the present invention, the present invention will be further described below in conjunction with specific examples, and the comprehensive performance of the present invention will be verified and analyzed by comparing with the reference airfoil.
[0093] The specific implementation process will be described below through an example of airfoil aerodynamic optimization as an example.
[0094] The purpose of the airfoil aerodynamic optimization problem is to improve the aerodynamic characteristics of the airfoil. The design variables of airfoil aerodynamic optimization problem are ten disturbance parameters of airfoil shape function. The optimized model expression is as follows:
[0095]
[0096] In the formula, Cl is the lift coefficient, Cd is the drag coefficient, and t max is the maximum thickness of the airfoil, is the maximum thickness of the initial airfoil, Cd 0 is the initial airfoil drag coeffic...
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