32th Congress of the International Council of the Aeronautical Sciences

04.2 - Aerostructures Design, Structural Dynamics, Aeroelasticity

AN INTEGRATED AERODYNAMIC/THERMAL/STRUCTURAL DESIGN FRAMEWORK FOR HYPERSONIC VEHICLES

C. Li¹, Z.Q. Wan¹, X. Wang¹; ¹Beihang University, China

It takes aerodynamic force, aerodynamic heating, heat transfer and structure deformation into account together, which can achieve a more realistic design during the preliminary design phase. An integrated optimization for aerodynamic shape parameters and structure sizes of the model in strictest results of aerothermoelastic analysis is performed to obtain the optimal design parameters.


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