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

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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 str...

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Detalles Bibliográficos
Clasificación:Libro Electrónico
Autor principal: Zender, George W. (Autor)
Autor Corporativo: United States. National Advisory Committee for Aeronautics
Otros Autores: Libove, Charles
Formato: Documento de Gobierno Electrónico eBook
Idioma:Inglés
Publicado: Washington, D.C. : National Advisory Committee for Aeronautics, [1948]
Colección:Technical note (United States. National Advisory Committee for Aeronautics) ; no. 1525.
Temas:
Box beams.
Strains and stresses > Measurement.
Bending.
Torsion.
Poutres-caissons.
Torsion (Mécanique)
box beams.
torsional stress.
Bending
Box beams
Strains and stresses > Measurement
Torsion
Acceso en línea:Texto completo

MARC

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100 1 |a Zender, George W.,  |e author. 
245 1 0 |a Stress and distortion measurements in a 45 degree swept box beam subjected to bending and to torsion /  |c by George Zender and Charles Libove. 
264 1 |a Washington, D.C. :  |b National Advisory Committee for Aeronautics,  |c [1948] 
300 |a 1 online resource (38 pages) :  |b illustrations 
336 |a text  |b txt  |2 rdacontent 
337 |a computer  |b c  |2 rdamedia 
338 |a online resource  |b cr  |2 rdacarrier 
490 1 |a National Advisory Committee for Aeronautics technical note ;  |v number 1525 
500 |a NACA TN No. 1525. 
504 |a Includes bibliographical references. 
520 3 |a 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. 
588 0 |a Print version record. 
590 |a Knovel  |b ACADEMIC - Aerospace & Radar Technology 
650 0 |a Box beams. 
650 0 |a Strains and stresses  |x Measurement. 
650 0 |a Bending. 
650 0 |a Torsion. 
650 6 |a Poutres-caissons. 
650 6 |a Torsion (Mécanique) 
650 7 |a box beams.  |2 aat 
650 7 |a torsional stress.  |2 aat 
650 7 |a Bending  |2 fast 
650 7 |a Box beams  |2 fast 
650 7 |a Strains and stresses  |x Measurement  |2 fast 
650 7 |a Torsion  |2 fast 
700 1 |a Libove, Charles. 
710 1 |a United States.  |b National Advisory Committee for Aeronautics. 
730 0 |a Technical Report Archive & Image Library (TRAIL) 
776 0 8 |i Print version:  |a Zender, George.  |t Stress and distortion measurements in a 45 degree swept box beam subjected to bending and to torsion  |w (OCoLC)656904291 
830 0 |a Technical note (United States. National Advisory Committee for Aeronautics) ;  |v no. 1525. 
856 4 0 |u https://appknovel.uam.elogim.com/kn/resources/kpSDMSBBS1/toc  |z Texto completo 
994 |a 92  |b IZTAP 

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