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150825s1933 dcua ob 000 0 eng d |
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|a KNOVL
|b eng
|e rda
|e pn
|c KNOVL
|d ZCU
|d UAB
|d DKU
|d OCLCQ
|d CEF
|d RRP
|d YOU
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|d OCLCO
|d OCLCQ
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|d OCLCQ
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|a 9781680156386
|q (electronic bk.)
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|a 1680156381
|q (electronic bk.)
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|a GBVCP
|b 856592293
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|a (OCoLC)919149686
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|a TL501
|b .U52 1933eb
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|a 629.4
|2 23
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|a UAMI
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|a Donnell, L. H.,
|e author.
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|a Stability of thin-walled tubes under torsion /
|c by L.H. Donnell.
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|a Washington, D.C. :
|b G.P.O.,
|c [1933]
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|a 1 online resource (24 pages) :
|b illustrations
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|a text
|b txt
|2 rdacontent
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|a computer
|b c
|2 rdamedia
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|a online resource
|b cr
|2 rdacarrier
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|a Report / National Advisory Committee for Aeronautics ;
|v number 479
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|a Includes bibliographical references.
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|a Print version record.
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|a In this report a theoretical solution is developed for the torsion on a round thin-walled tube for which the walls become unstable. The results of this theory are given by a few simple formulas and curves which cover all cases. The differential equations of equilibrium are derived in a simpler form than previously found, it being shown that many items can be neglected. --
|c Provided by publisher.
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|a Knovel
|b ACADEMIC - Aerospace & Radar Technology
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|a Aeronautics
|x Research.
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|a Aéronautique
|x Recherche.
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|a Aeronautics
|x Research.
|2 fast
|0 (OCoLC)fst00798376
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|a United States.
|b National Advisory Committee for Aeronautics.
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|i Print version:
|a Donnell, L.H.
|t Stability of thin-walled tubes under torsion
|w (OCoLC)46820191
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|a Report (United States. National Advisory Committee for Aeronautics) ;
|v no. 479.
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856 |
4 |
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|u https://appknovel.uam.elogim.com/kn/resources/kpSTWTTNA3/toc
|z Texto completo
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|a 92
|b IZTAP
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