FEASIBILITY OF JOINING ADVANCED COMPOSITE FLIGHT VEHICLE STRUCTURES.
Quarterly progress rept. no. 1, 1 May-31 Jul 66,
IIT RESEARCH INST CHICAGO IL MECHANICS OF MATERIALS RESEARCH DIV
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The purpose of this study is to establish the feasibility of using rational engineering methods to design bonded and mechanically fastened joints fabricated from composite and composite-metal adherends. Work during this quarter has concentrated on Literature Survey and selection and computer programming of analytical expressions to be used in the design methods. Author
- Couplers, Fasteners and Joints