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Experimental data on single-bolt joints in quasi isotropic graphite/polyimide laminatesSixteen ply, quasi-isotropic laminates of Celanese Celion 6000/PMR-15 and Celion 6000/LARC-160 with a fiber orientation of (0/45/90/-45) sub 2S were evaluated. Tensile and open hole specimens were tested at room temperature to establish laminate tensile strength and net tensile strength at an unloaded bolt hole. Double lap joint specimens with a single 4.83-mm (0.19 in.) diameter bolt torqued to 1.7 N-m (15 lbf-in.) were tested in tension at temperatures of 116 K (-250F), 297 K (75F), and 589 K (600F). The joint ratios of w/d (specimen width to hole diameter) and e/d (edge distance to hole diameter) were varied from 4 to 6 and from 2 to 4, respectively. The effect of joint geometry and temperature on failure mode and joint stresses are shown. Joint stresses calculated at maximum load for each joint geometry and test temperature are reported. Joint strength in net tension, bearing, and shear out at 116 K (-250F), 297 K (75F), and 589 K (600F) are given for the Celion 6000/PMR-15 and Celion 6000/LARC-160 laminates.
Document ID
19820017449
Acquisition Source
Legacy CDMS
Document Type
Technical Publication (TP)
Authors
Wichorek, G. R.
(NASA Langley Research Center Hampton, VA, United States)
Date Acquired
September 4, 2013
Publication Date
May 1, 1982
Subject Category
Composite Materials
Report/Patent Number
NASA-TP-2015
NAS 1.60:2015
L-15103
Report Number: NASA-TP-2015
Report Number: NAS 1.60:2015
Report Number: L-15103
Accession Number
82N25325
Funding Number(s)
PROJECT: RTOP 506-53-23-06
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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