SUN Yan, HUANG Yong, WANG Yuntao, MENG Dehong, WANG Hao. Development and precision validation of static aeroelastic computational module on flow solver TRIP[J]. ACTA AERODYNAMICA SINICA, 2017, 35(5): 620-624. DOI: 10.7638/kqdlxxb-2015.0154
Citation: SUN Yan, HUANG Yong, WANG Yuntao, MENG Dehong, WANG Hao. Development and precision validation of static aeroelastic computational module on flow solver TRIP[J]. ACTA AERODYNAMICA SINICA, 2017, 35(5): 620-624. DOI: 10.7638/kqdlxxb-2015.0154
shu

Development and precision validation of static aeroelastic computational module on flow solver TRIP

  • 1.

    State Key Laboratory of Aerodynamics, China Aerodynamics Research and Development Center, Mianyang 621000, China

  • 2.

    Computational Aerodynamics Institute of China Aerodynamics Research and Development Center, Mianyang 621000, China

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  • Received Date: August 25, 2015
  • Revised Date: October 13, 2015
  • Available Online: January 07, 2021
    Graphical Abstract
    • Abstract
  • A static aeroelastic computational module is developed on the flow solver TRIP. Firstly, the frame, main component units and coupling strategy of the static aeroelastic computational module are introduced briefly. Then numerical methods used in the component units are described in detail. Finally, the static aeroelastic computational module is tested and validated through three cases:high respect-ratio wing, DLR-F6 wing-body model and HIRENASD wing model. The computational results of high respect-ratio wing show that flexible matrix method, modal superposition method and finite element method can have same deformation results when the structure modes are selected properly. The result consistency of DLR-F6 or HIRENASD model among different solvers demonstrates that the static aeroelastic computational module has adopted a correct algorithm procedure. The results consistency of DLR-F6 or HIRENASD model between computations and tests shows that the present static aeroelastic computational module has a good prediction precision.
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    • References (18)
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