Method of attachment and effects of joining method are of equal importance to selection of materials; joining design problems arising from inadequate consideration of practical factors are shown; examples are given ranging from WW II aircraft (collection of holes held together with fasteners) to space vehicles' fastening system; examples relate to re-entry body test structure requiring use of multilayered construction, joining problem involving cryogenic temperature, and heat sink leading edge attachment of X-15 aircraft.
Joining -- Real challenge in use of advanced structures
SAE -- Paper
SAE Meeting ; 1965 Fasteners
1965
9 pages
Conference paper
English
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