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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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Detalles Bibliográficos
Clasificación:Libro Electrónico
Autor principal: Wagner, Herbert, 1900-1982
Autor Corporativo: United States. National Advisory Committee for Aeronautics
Formato: Documento de Gobierno Electrónico eBook
Idioma:Inglés
Publicado: Washington, D.C. : National Advisory Committee for Aeronautics, [1931]
Colección:Technical memorandums (United States. National Committee for Aeronautics) ; no. 606.
Temas:
Acceso en línea:Texto completo

MARC

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086 0 |a Y 3.N 21/5:8/606 
088 |a NACA-TM-606 
049 |a UAMI 
100 1 |a Wagner, Herbert,  |d 1900-1982. 
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. 
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. 
588 0 |a Print version record. 
504 |a Includes bibliographical references. 
538 |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 
583 1 |a digitized  |c 2011  |h University of North Texas  |l committed to preserve  |2 pda  |5 TXdn. 
590 |a Knovel  |b ACADEMIC - Aerospace & Radar Technology 
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. 
650 6 |a Tôle. 
650 6 |a Poutres. 
650 6 |a Mathématiques. 
650 6 |a Étrésillons. 
650 6 |a Contraintes (Mécanique) 
650 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 |a 92  |b IZTAP