Simulation and Analysis of Fluid-Solid-Thermal Unidirectional Coupling of Near-Space Airship

Based on the biaxial experiment data of the membrane material under hot and cold conditions, the mechanical properties calculation model of envelope material was established with consideration of the effects of varying stress ratios, stress magnitudes and temperatures on the mechanical properties of near-space airship material. Using the heat source model, Computational Fluid Dynamics (CFD) simulation, User-Defined Function (UDF), structural finite element analysis software and the user subroutine of an airship to define the behaviour of fabric material, the fluid-structure-thermal coupling model of airship envelopes was established. In addition, a near-space airship was selected as the research subject to calculate the diurnal temperature differences during the summer solstice and analyse the diurnal temperature distribution of the envelope. Under controlled environmental conditions, the deformation law of the near-space airship under the influence of fluid-structure-thermal coupling was calculated and summarised. The present fluid-solid-thermal coupling model takes into account the anisotropy of materials, temperature, stress magnitude, stress ratio and other influencing factors, which can more accurately reflect and predict the stress-strain distribution and the deformation law of near-space airships.

Automated summary

This study establishes a mechanical properties calculation model for near-space airship envelope materials, taking into account the effects of stress ratios, stress magnitudes, and temperatures. By using various simulation and analysis techniques, the fluid-structure-thermal coupling model of airship envelopes is developed, allowing for a more accurate prediction of stress-strain distribution and deformation characteristics.