Abstract
The article presents a mathematical model of the dynamics of the canopy of an axisymmetric parachute taking into account the biaxiality of the state of complex stress of the tissue, the effect of the rigging lines of the annular carcass, viscous deformation, riffling. For the solution a threelayered symmetric implicit difference schema is suggested. The method of accelerated attainment of a stable solution without distortion of the dynamic pattern is explained.
Talk to us
Join us for a 30 min session where you can share your feedback and ask us any queries you have
Schedule a callDisclaimer: All third-party content on this website/platform is and will remain the property of their respective owners and is provided on "as is" basis without any warranties, express or implied. Use of third-party content does not indicate any affiliation, sponsorship with or endorsement by them. Any references to third-party content is to identify the corresponding services and shall be considered fair use under The CopyrightLaw.
