Flat sheet metal girder with very thin metal web : Part 2 : Sheet metal girders with spars resistant to bending - oblique uprights - stiffness

Noting that the stiffness of the girder increases very rapidly as Beta increases, the result can be summed up as follows: When the cross stress preponderates in one direction and when the web plate is to be given the dimensions commensurate to its stresses, it is advisable (regardless of any ensuing...

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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. 605.
Subjects:
Sheet-metal.
Girders.
Mathematics.
Struts (Engineering)
Bending.
elektronické knihy
electronic books
ISBN: 9781680156591
1680156594
Physical Description: 1 online resource (38, [6] pages) : illustrations

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Table of contents

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003 OCoLC
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006 m o d
007 cr cn|||||||||
008 150728s1931 dcua ot f000 0 eng d
040 |a SINTU  |b eng  |e pn  |c SINTU  |d 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 9781680156591  |q (electronic bk.) 
020 |a 1680156594  |q (electronic bk.) 
035 |a (OCoLC)914568933  |z (OCoLC)951668825  |z (OCoLC)1363847327 
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 2 : Sheet metal girders with spars resistant to bending - oblique uprights - stiffness /  |c Herbert Wagner. 
260 |a Washington, D.C. :  |b National Advisory Committee for Aeronautics,  |c [1931] 
300 |a 1 online resource (38, [6] 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 605 
500 |a "February, 1931." 
500 |a NACA TM No. 605. 
500 |a Translated from Zeitschrift fur Flugtechnik und Motorluftschiffahrt. Vol. 20, No. 9, May 14, No. 10, May 28, and No. 11, June 14, 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 Noting that the stiffness of the girder increases very rapidly as Beta increases, the result can be summed up as follows: When the cross stress preponderates in one direction and when the web plate is to be given the dimensions commensurate to its stresses, it is advisable (regardless of any ensuing structural difficulties) to set the uprights at about Beta = 120 degrees, thereby lowering the weight of the plate wall 15 percent (in contrast to Beta = 90 degrees), and raising the stiffness 55 percent. But, when the cross stresses alternate and are approximately of the same intensity in both directions, or, if the web plate thickness is determined by other structural reasons, then Beta = 90 degrees should be chosen. 
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 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)695044344 
830 0 |a Technical memorandums (United States. National Committee for Aeronautics) ;  |v no. 605. 
856 4 0 |u https://proxy.k.utb.cz/login?url=https://app.knovel.com/hotlink/toc/id:kpFSMGVT07/flat-sheet-metal?kpromoter=marc  |y Full text 

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