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KNOVEL_ocn919130291 |
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20231027140348.0 |
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150825s1950 dcua obt f000 0 eng d |
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|a KNOVL
|b eng
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|c KNOVL
|d ZCU
|d UAB
|d DKU
|d OCLCQ
|d CEF
|d RRP
|d YOU
|d S2H
|d OCLCO
|d COP
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|d OCLCQ
|d UPM
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|a 9781680156171
|q (electronic bk.)
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|a 1680156179
|q (electronic bk.)
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|a GBVCP
|b 856592196
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|a (OCoLC)919130291
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|a TA660.P6
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|a 624.17765
|2 23
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|a Y 3.N 21/5:6/2073
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|a UAMI
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|a Stowell, Elbridge Z.,
|e author.
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|a Stress and strain concentration at a circular hole in an infinite plate /
|c Elbridge Z. Stowell.
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|a Washington, D.C. :
|b National Advisory Committee for Aeronautics,
|c 1950.
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|a 1 online resource (14 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 National Advisory Committee for Aeronautics ;
|v number 2073
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|a "April 1950."
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|a NACA TN No. 2073.
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|a Includes bibliographical references.
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|a Formulas for stress and strain concentration at a circular hole in an infinite plate under tension have been derived for use in the plastic region. Values of stress concentration obtained from the formula are in good agreement with limited tests on 24S-T3 aluminum-alloy tension panels. The strain concentration factor is also in agreement with these tests.
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|a Print version record.
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|a Knovel
|b ACADEMIC - Aerospace & Radar Technology
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|a Plates (Engineering)
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|a Holes.
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|a Strains and stresses.
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|a Plaques (Ingénierie)
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|a Trous.
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|a Contraintes (Mécanique)
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|a stress.
|2 aat
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|a strain.
|2 aat
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|a Holes
|2 fast
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|a Plates (Engineering)
|2 fast
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|a Strains and stresses
|2 fast
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|a United States.
|b National Advisory Committee for Aeronautics.
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|a Technical Report Archive & Image Library (TRAIL)
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|i Print version:
|a Stowell, Elbridge Z.
|t Stress and strain concentration at a circular hole in an infinite plate
|w (OCoLC)662764206
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|a Technical note (United States. National Advisory Committee for Aeronautics) ;
|v no. 2073.
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|u https://appknovel.uam.elogim.com/kn/resources/kpSSCCHIP3/toc
|z Texto completo
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|a 92
|b IZTAP
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