Flexibility Equations for Active Rack Isolation System Umbilicals with Planar End Loading

Hampton et al developed equations for the in-plane deflections and flexibilities of an idealized umbilical under terminal in-plane loading. The effect of gravity can be neglected due to the on-orbit application.

Saved in:
Bibliographic Details
Published in:AIAA journal 2001-10, Vol.39 (10), p.2024-2027
Main Authors: Hampton, R. David, Quraishi, Naveed, Rupert, Jason K
Format: Article
Language:English
Subjects:
Cantilever beams
Deflection (structures)
Elasticity
Exact sciences and technology
Flexible structures
Fundamental areas of phenomenology (including applications)
Gravitational effects
Gravity
Mathematical models
Mechanical engineering
Numerical analysis
Optimization
Physics
Solid mechanics
Space stations
Static elasticity
Static elasticity (thermoelasticity...)
Stiffness
Structural and continuum mechanics
Citations: Items that this one cites
Items that cite this one
Online Access:Get full text
Tags: Add Tag
No Tags, Be the first to tag this record!
Description
Summary:Hampton et al developed equations for the in-plane deflections and flexibilities of an idealized umbilical under terminal in-plane loading. The effect of gravity can be neglected due to the on-orbit application.
ISSN:0001-1452
1533-385X
DOI:10.2514/2.1197