Advanced FSI model of parachute decelerator
The result's identifiers
Result code in IS VaVaI
<a href="https://www.isvavai.cz/riv?ss=detail&h=RIV%2F00216305%3A26210%2F22%3APR36113" target="_blank" >RIV/00216305:26210/22:PR36113 - isvavai.cz</a>
Result on the web
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DOI - Digital Object Identifier
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Alternative languages
Result language
angličtina
Original language name
Advanced FSI model of parachute decelerator
Original language description
The numerical model which consists of detailed models of parachute canopy in the geometrical representation of CAD model, a surface mesh of canopy and volume mesh of flow domain simulation atmosphere. Fluid-structure simulation parameters and physical models are used, based on LS-Dyna and Ansys Fluent codes use. The computational model shall deliver loads on structure (tissue, sews, slinges and ropes), drag and side forces, decelerations, steady descent speed. It should be used as a design tool for checking changes in design with a reasonable turnaround time for the detailed design of the parachute canopy.
Czech name
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Czech description
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Classification
Type
O - Miscellaneous
CEP classification
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OECD FORD branch
20304 - Aerospace engineering
Result continuities
Project
<a href="/en/project/TN01000029" target="_blank" >TN01000029: National Competence Centre for Aeronautics and Space</a><br>
Continuities
P - Projekt vyzkumu a vyvoje financovany z verejnych zdroju (s odkazem do CEP)
Others
Publication year
2022
Confidentiality
S - Úplné a pravdivé údaje o projektu nepodléhají ochraně podle zvláštních právních předpisů