Stress and distortion analysis of a swept box beam having bulkheads perpendicular to the spars

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Bibliographic Details
Main Author Heldenfels, Richard R. (Author)
Corporate Author United States. National Advisory Committee for Aeronautics
Other Authors Zender, George W., Libove, Charles
Format Electronic eBook
LanguageEnglish
Published Washington, D.C. : National Advisory Committee for Aeronautics, 1950.
SeriesTechnical note (United States. National Advisory Committee for Aeronautics) ; no. 2232.
Subjects
Box beams.
Bulkheads.
Strains and stresses.
Structural analysis (Engineering)
elektronické knihy
electronic books
Online AccessFull text
ISBN9781680156188
1680156187
Physical Description1 online resource (90 pages) : illustrations

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Abstract:A method is presented for the approximate calculation of the stresses and distortions in a box beam representing the main structural component of a swept wing with a carry-through section and with bulkheads perpendicular to the spars. The application of the method is illustrated by a numerical example and its results are compared with previously published test data.
Item Description:Date of issue: November 1950.
Report no. NACA-TN-2232
Bibliography:Includes bibliographical references.
ISBN:9781680156188
1680156187
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 (90 pages) : illustrations

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