Flat sheet metal girder with very thin metal web : Part 3 : Sheet metal girders with spars resistant to bending - the stress in uprights - diagonal tension fields

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 in...

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Bibliographic Details
Main Author: Wagner, Herbert, 1900-1982.
Corporate Author: United States. National Advisory Committee for Aeronautics.
Format: eBook
Language: English
Published: Washington, D.C. : National Advisory Committee for Aeronautics, [1931]
Series: Technical memorandums (United States. National Committee for Aeronautics) ; no. 606.
Subjects:
Sheet-metal.
Girders.
Mathematics.
Struts (Engineering)
Strains and stresses.
Bending.
elektronické knihy
electronic books
ISBN: 9781680156584
1680156586
Physical Description: 1 online resource (39, [8] pages) : illustrations

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Table of contents

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001 kn-ocn914554301
003 OCoLC
005 20240717213016.0
006 m o d
007 cr cn|||||||||
008 150727s1931 dcua ot f000 0 eng d
040 |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  |d OCLCL  |d SXB 
020 |a 9781680156584  |q (electronic bk.) 
020 |a 1680156586  |q (electronic bk.) 
035 |a (OCoLC)914554301  |z (OCoLC)951668994  |z (OCoLC)1363847328 
100 1 |a Wagner, Herbert,  |d 1900-1982.  |1 https://id.oclc.org/worldcat/entity/E39PBJxCBtWVWGQhGqFwfBg3Qq 
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. 
260 |a Washington, D.C. :  |b National Advisory Committee for Aeronautics,  |c [1931] 
300 |a 1 online resource (39, [8] 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 Technical memorandums / National Advisory Committee for Aeronautics ;  |v 606 
500 |a "February, 1931." 
500 |a NACA TM No. 606. 
500 |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. 
506 |a Plný text je dostupný pouze z IP adres počítačů Univerzity Tomáše Bati ve Zlíně nebo vzdáleným přístupem pro zaměstnance a studenty 
520 3 |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. 
504 |a Includes bibliographical references. 
590 |a Knovel  |b Knovel (All titles) 
650 0 |a Sheet-metal. 
650 0 |a Girders. 
650 0 |a Mathematics. 
650 0 |a Struts (Engineering) 
650 0 |a Strains and stresses. 
650 0 |a Bending. 
655 7 |a elektronické knihy  |7 fd186907  |2 czenas 
655 9 |a electronic books  |2 eczenas 
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://proxy.k.utb.cz/login?url=https://app.knovel.com/hotlink/toc/id:kpFSMGVTM1/flat-sheet-metal?kpromoter=marc  |y Full text 

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