Treffer: Fluid-structure interaction modelling of parachute soft-landing dynamics
Title:
Fluid-structure interaction modelling of parachute soft-landing dynamics
Source:
Advances and challenges in flow simulation and modelling: minisymposium at the 5th World Congress on Computational Mechanics, July 7-12, 2002, Vienna, AustriaInternational journal for numerical methods in fluids. 47(6-7):619-631
Publisher Information:
Chichester: Wiley, 2005.
Publication Year:
2005
Physical Description:
print, 23 ref
Original Material:
INIST-CNRS
Subject Terms:
Mechanics acoustics, Mécanique et acoustique, Sciences exactes et technologie, Exact sciences and technology, Physique, Physics, Domaines classiques de la physique (y compris les applications), Fundamental areas of phenomenology (including applications), Mécanique des solides, Solid mechanics, Mécanique des structures et des milieux continus, Structural and continuum mechanics, Vibration, onde mécanique, stabilité dynamique (aéroélasticité, contrôle vibration...), Vibration, mechanical wave, dynamic stability (aeroelasticity, vibration control...), Mécanique des fluides, Fluid dynamics, Méthodes de calcul en mécanique des fluides, Computational methods in fluid dynamics, Vibrations and mechanical waves, Atterrissage, Landing, Aterrizaje, Champ écoulement, Flow pattern, Génération maille, Mesh generation, Interaction fluide structure, Fluid-structure interactions, Modélisation, Modelling, Mécanique fluide numérique, Computational fluid dynamics, Parachute, Parachutes, Simulation numérique, Digital simulation, Trajectoire, Trajectories, flow simulation, fluid-structure interactions, parachute aerodynamics, soft landing
Document Type:
Konferenz
Conference Paper
File Description:
text
Language:
English
Author Affiliations:
Department of Physics, Bethel University, St. Paul, MN, 55112, United States
Mechanical Engineering, Rice University, MS 321, 6100 Main Street, Houston, TX 77005, United States
U.S. Army Natick Soldier Center, Kansas Street, Natick, MA, 10760, United States
Mechanical Engineering, Rice University, MS 321, 6100 Main Street, Houston, TX 77005, United States
U.S. Army Natick Soldier Center, Kansas Street, Natick, MA, 10760, United States
ISSN:
0271-2091
Rights:
Copyright 2005 INIST-CNRS
CC BY 4.0
Sauf mention contraire ci-dessus, le contenu de cette notice bibliographique peut être utilisé dans le cadre d’une licence CC BY 4.0 Inist-CNRS / Unless otherwise stated above, the content of this bibliographic record may be used under a CC BY 4.0 licence by Inist-CNRS / A menos que se haya señalado antes, el contenido de este registro bibliográfico puede ser utilizado al amparo de una licencia CC BY 4.0 Inist-CNRS
CC BY 4.0
Sauf mention contraire ci-dessus, le contenu de cette notice bibliographique peut être utilisé dans le cadre d’une licence CC BY 4.0 Inist-CNRS / Unless otherwise stated above, the content of this bibliographic record may be used under a CC BY 4.0 licence by Inist-CNRS / A menos que se haya señalado antes, el contenido de este registro bibliográfico puede ser utilizado al amparo de una licencia CC BY 4.0 Inist-CNRS
Notes:
Physics: fluid mechanics
Physics: solid mechanics
Physics: solid mechanics
Accession Number:
edscal.16594203
Database:
PASCAL Archive
Weitere Informationen
Soft landing of a payload with the aid of a retraction device is an important aspect in cargo parachute operations. Accurate simulation of this class of parachute operations with a computer model that takes into account the fluid-structure interactions involved would complement drop tests and support the design of cargo parachute systems. We describe the computational methods developed for this purpose, demonstrate how the computational model works in investigation of different soft-landing conditions.