Honeycomb Sandwich Joints for Primary Structure

descriptionPublicationkeyboard_double_arrow_right Article , Other literature type 12 May 1980 English Publisher:American Institute of Aeronautics and Astronautics (AIAA)Journal:Journal of Aircraft, volume 18, pages 770-774 (issn: 0021-8669, eissn: 1533-3868,

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Authors: U. SOUDAK; R. HAMM;

doi: 10.2514/3.57561 , 10.2514/6.1980-780

Honeycomb Sandwich Joints for Primary Structure

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Abstract

Analysis methods and joint design details h ave b een developed for adhesively bonded aluminum h oneycomb i n aircraft primary structure. Joint d esign d etails, which were tested f or strength, durability and e nvironmental resistance, p rovide

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Boeing (United States)
United States

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