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Strength of adhesive-bonded hybrid structuresStructures prepared from materials with different thermal and mechanical properties by means of fiber-strengthened binders can fail in a number of ways. The present lecture is focused on failures through debonding at the metal or at the fiber-reinforced plastic. A method for calculating the stress distribution in adhesive layers as a function of the load is outlined, and its usefulness in providing insight into the behavior of bonds in hybrid structures is noted. Means of eliminating the unfavorable effects of temperature, humidity, creep and relaxation on the bonds in the manufacture of hybrid structures are examined, along with test methods developed for such structures.
Document ID
19790023430
Acquisition Source
Legacy CDMS
Document Type
Technical Memorandum (TM)
Authors
Kirschke, L.
(NASA Headquarters Washington, DC United States)
Prinz, R.
(NASA Headquarters Washington, DC United States)
Schnell, H.
(NASA Headquarters Washington, DC United States)
Date Acquired
September 3, 2013
Publication Date
June 1, 1979
Subject Category
Mechanical Engineering
Report/Patent Number
NASA-TM-75488
DGLR-PAPER-78-180
Report Number: NASA-TM-75488
Report Number: DGLR-PAPER-78-180
Accession Number
79N31601
Funding Number(s)
CONTRACT_GRANT: NASW-3199
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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