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20231027140348.0 |
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150727s1931 dcua ot f000 0 eng d |
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|a SINTU
|b eng
|e pn
|c SINTU
|d KNOVL
|d ZCU
|d TJC
|d OCLCQ
|d UAB
|d COO
|d DKU
|d OCLCQ
|d CEF
|d RRP
|d YOU
|d S2H
|d OCLCO
|d OCLCQ
|d OCLCO
|d OCLCQ
|d TRAAL
|d OCLCO
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019 |
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|a 951668994
|a 1363847328
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|a 9781680156584
|q (electronic bk.)
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|a 1680156586
|q (electronic bk.)
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|a GBVCP
|b 856591750
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|a (OCoLC)914554301
|z (OCoLC)951668994
|z (OCoLC)1363847328
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|a TA460
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082 |
0 |
4 |
|a 620.166
|2 23
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|a Y 3.N 21/5:8/606
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088 |
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|a NACA-TM-606
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|a UAMI
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100 |
1 |
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|a Wagner, Herbert,
|d 1900-1982.
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245 |
1 |
0 |
|a Flat sheet metal girder with very thin metal web :
|b Part 3 : Sheet metal girders with spars resistant to bending - the stress in uprights - diagonal tension fields /
|c Herbert Wagner.
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260 |
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|a Washington, D.C. :
|b National Advisory Committee for Aeronautics,
|c [1931]
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300 |
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|a 1 online resource (39, [8] pages) :
|b illustrations
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336 |
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|a text
|b txt
|2 rdacontent
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337 |
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|a computer
|b c
|2 rdamedia
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338 |
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|a online resource
|b cr
|2 rdacarrier
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490 |
1 |
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|a Technical memorandums / National Advisory Committee for Aeronautics ;
|v 606
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500 |
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|a "February, 1931."
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500 |
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|a NACA TM No. 606.
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500 |
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|a Translated from Zeitschrift fur Flugtechnik und Motorluftschiffahrt. Vol. 20, No. 11, pp. 281-284, June 14, and No. 12, pp. 306-314, June 28, 1929, by the National Advisory Committee for Aeronautics.
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520 |
3 |
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|a This report continues the work presented in NACA-TM 605 and expands the scope to include the change in specific number of wrinkles from direction x to z, so that b and f become variable in direction z. Moreover, it seems likely that b and f increase from the edge toward the center if the sheet is infinitely thin.
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588 |
0 |
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|a Print version record.
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504 |
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|a Includes bibliographical references.
|
538 |
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|a Master and use copy. Digital master created according to Technical Guidelines for Digitizing Archival Materials for Electronic Access. U.S. National Archives and Records Administration, 2004.
|u http://www.archives.gov/preservation/technical/guidelines.html
|5 TxDN
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583 |
1 |
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|a digitized
|c 2011
|h University of North Texas
|l committed to preserve
|2 pda
|5 TXdn.
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590 |
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|a Knovel
|b ACADEMIC - Aerospace & Radar Technology
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650 |
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0 |
|a Sheet-metal.
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650 |
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0 |
|a Girders.
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650 |
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0 |
|a Mathematics.
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650 |
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0 |
|a Struts (Engineering)
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650 |
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0 |
|a Strains and stresses.
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650 |
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0 |
|a Bending.
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650 |
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6 |
|a Tôle.
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650 |
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6 |
|a Poutres.
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650 |
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6 |
|a Mathématiques.
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650 |
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6 |
|a Étrésillons.
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650 |
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6 |
|a Contraintes (Mécanique)
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650 |
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7 |
|a sheet metal.
|2 aat
|
650 |
|
7 |
|a mathematics.
|2 aat
|
650 |
|
7 |
|a applied mathematics.
|2 aat
|
650 |
|
7 |
|a strain.
|2 aat
|
650 |
|
7 |
|a stress.
|2 aat
|
650 |
|
7 |
|a Bending
|2 fast
|
650 |
|
7 |
|a Girders
|2 fast
|
650 |
|
7 |
|a Mathematics
|2 fast
|
650 |
|
7 |
|a Sheet-metal
|2 fast
|
650 |
|
7 |
|a Strains and stresses
|2 fast
|
650 |
|
7 |
|a Struts (Engineering)
|2 fast
|
710 |
1 |
|
|a United States.
|b National Advisory Committee for Aeronautics.
|
776 |
0 |
8 |
|i Print version:
|a Wagner, Herbert.
|t Flat sheet metal girder with very thin metal web.
|d Washington, D.C. : National Advisory Committee for Aeronautics ; [1931]
|w (OCoLC)695046495
|
830 |
|
0 |
|a Technical memorandums (United States. National Committee for Aeronautics) ;
|v no. 606.
|
856 |
4 |
0 |
|u https://appknovel.uam.elogim.com/kn/resources/kpFSMGVTM1/toc
|z Texto completo
|
994 |
|
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|a 92
|b IZTAP
|