Fluid–structure interaction and flight dynamics analysis of parachute–payload system during uncontrolled airdrop process

The coupling behaviors of a special parachute’s inflation incorporating fluid–structure interaction and flight dynamics are investigated based on the multibody dynamic model and LS-DYNA nonlinear analysis code. A new coupling model is developed to predict both the opening phase of parachute and the...

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Bibliographic Details
Published in:Proceedings of the Institution of Mechanical Engineers. Part G, Journal of aerospace engineering Journal of aerospace engineering, 2018-10, Vol.232 (13), p.2499-2512
Main Authors: Gao, Xinglong, Zhang, Qingbin, Tang, Qiangang
Format: Article
Language:English
Subjects:
Aerodynamics
Computer simulation
Coupling
Data transfer (computers)
Dynamic characteristics
Dynamic models
Finite element method
Fluid-structure interaction
Missions
Multibody systems
Nonlinear analysis
Parachute inflation
Trajectories
Unsteady flow
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Summary:The coupling behaviors of a special parachute’s inflation incorporating fluid–structure interaction and flight dynamics are investigated based on the multibody dynamic model and LS-DYNA nonlinear analysis code. A new coupling model is developed to predict both the opening phase of parachute and the trajectory of payload during airdrop mission in low attitude. The moving mesh technology is introduced to realize the finite mass inflation simulation. A simplified integration platform is built by coupling the fluid–structure interaction and flight dynamics model, and solved based on two-way data transfer to efficiently replicate the dynamic characteristics of parachute finite mass inflation. Finally, the opening performances of the parachute at different airdropping velocities are analyzed and compared with the experimental results. The unsteady flow dynamics is simulated and the wake re-contacts phenomenon occurred. Taking consideration of the periodical disturb of wind gust, the trajectory of parachute–payload system is simulated and compared with the real airdrop test results. In conclusion, the results show that this coupling model is efficient to simulate and predict the dynamics behaviors of parachute–payload system in a finite mass inflation scenario, which will be beneficial for airdrop missions.
ISSN:0954-4100
2041-3025
DOI:10.1177/0954410017718565