Vasily V. Chedrik, Sergey A. Tuktarov

DOI Number: N/A

Conference number: IFASD-2015-055

An evolutionary approach to synthesis of optimal aircraft component layouts has been developed. It is based on combined application of topology optimization, an engineering interpretation and optimum sizing of load-bearing structural elements. The developed approach gives possibility to include stress, buckling and aeroelasticity constraints altogether in unified design procedure and to get an optimal wing structure.

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In Categories: 2. IFASD 2015, Aeroelastic Optimisation
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