Stress and distortion measurements in a 45 degree swept box beam subjected to bending and to torsion

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Bibliographic Details
Main Author Zender, George W. (Author)
Corporate Author United States. National Advisory Committee for Aeronautics
Other Authors Libove, Charles
Format Electronic eBook
LanguageEnglish
Published Washington, D.C. : National Advisory Committee for Aeronautics, [1948]
SeriesTechnical note (United States. National Advisory Committee for Aeronautics) ; no. 1525.
Subjects
Online AccessFull text
ISBN9781680156133
1680156136
Physical Description1 online resource (38 pages) : illustrations

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Abstract:An untapered aluminum-alloy box beam, representing the main structural component of a full-span, two-spar, 45 degree swept wing with a carry-through bay, was subjected to tip bending and twisting loads and its stresses and distortions were meaured. Only symmetrical loading was considered and the stresses were kept below the proportional limit.
Item Description:NACA TN No. 1525.
Bibliography:Includes bibliographical references.
ISBN:9781680156133
1680156136
Access:Plný text je dostupný pouze z IP adres počítačů Univerzity Tomáše Bati ve Zlíně nebo vzdáleným přístupem pro zaměstnance a studenty
Physical Description:1 online resource (38 pages) : illustrations