NASA Logo

NTRS

NTRS - NASA Technical Reports Server

Press Enter or click the Search button to begin your search.

Back to Results
Improved Joint Design for Box-Stiffened PanelsMass and strength analyses and system requirements identified titanium-box-stiffened-skin wall candidate for lightweight fuselage of pressurized vehicle. Photoelastic models of stiffener-to-skin joint used to identify quickly modifications to joint that lowers severity of stress concentration. Results with various photoelastic models cut from polyurethane sheet led to novel diffusion-bond joint with reduced stress concentration.
Document ID
19860000472
Acquisition Source
Legacy CDMS
Document Type
Other - NASA Tech Brief
Authors
Davis, R. C.
(PRC Kentron, Inc.)
Moses, P. L.
Date Acquired
August 12, 2013
Publication Date
September 1, 1986
Publication Information
Publication: NASA Tech Briefs
Volume: 10
Issue: 5
ISSN: 0145-319X
Subject Category
Fabrication Technology
Report/Patent Number
ISSN: 0145-319X
Report Number: LAR-13460
LAR-13460
Accession Number
86B10472
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.

Available Downloads

There are no available downloads for this record.
No Preview Available