Yabin Wang
ABSTRACT
Hypersonic vehicles1 have strong aerodynamic heating effect and structural deformation. Moreover, the aerodynamic heating and the heat conduction will change the structure temperature and material properties. In order to solve the flight characteristics of hypersonic vehicle accurately, it is very important to study its aerothermoelastic characteristics. Considering the complexity of the aerothermoelastic calculation process, a set of parallel aerothermoelastic calculation software is designed and developed, which can effectively carry out parallel computation and has a friendly software interface. Finally, by calculating and analyzing the thermal flutter characteristics of the triangular thin wing, the accuracy and applicability of the software developed in this paper are illustrated.
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Index Terms
- Design and Development of Parallel Computation Software for Aerothermoelasticity
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