NASA Logo

NTRS

NTRS - NASA Technical Reports Server

Collections About News Help Login
Back to Results
Verifying Stiffness Parameters Of Filament-Wound CylindersPredicted engineering stiffness parameters of filament-wound composite-material cylinders verified with respect to experimental data, by use of equations developed straightforwardly from applicable formulation of Hooke's law. Equations derived in engineering study of filament-wound rocket-motor cases, also applicable to other cylindrical pressure vessels made of orthotropic materials.
Document ID
19940000258
Acquisition Source
Legacy CDMS
Document Type
Other - NASA Tech Brief
Authors
Verderaime, V. (NASA Marshall Space Flight Center, Huntsville, AL.)
Rheinfurth, M. (NASA Marshall Space Flight Center, Huntsville, AL.)
Date Acquired
August 16, 2013
Publication Date
May 1, 1994
Publication Information
Publication: NASA Tech Briefs
Volume: 18
Issue: 5
ISSN: 0145-319X
Subject Category
Electronic Systems
Report/Patent Number
MFS-28626
Accession Number
94B10258
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.

Available Downloads

There are no available downloads for this record.

Related Records

IDRelationTitleN83-16400/TBSee AlsoIdentification And Management Of Filament-Wound Case Stiffness Parameters.
No Preview Available