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The strength and stiffness of shear webs with round lightening holes having 45 degree flanges /

Tests were made of 18 shear webs with round lightening holes having 45 degree flanges. The purpose of the tests was to extend the range of a previous investigation to larger ratios of hole diameter to web depth and of web depth to web thickness. Simple empirical formulas are given for the strength a...

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Detalles Bibliográficos
Clasificación:Libro Electrónico
Autor principal: Kuhn, Paul (Autor)
Autores Corporativos: United States. National Advisory Committee for Aeronautics, Langley Aeronautical Laboratory
Formato: Documento de Gobierno Electrónico eBook
Idioma:Inglés
Publicado: Washington, D.C. : National Advisory Committee for Aeronautics, [1942]
Colección:Wartime Reports (United States. National Advisory Committee for Aeronautics) ; no. L323.
Temas:
Acceso en línea:Texto completo

MARC

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049 |a UAMI 
100 1 |a Kuhn, Paul,  |e author. 
245 1 4 |a The strength and stiffness of shear webs with round lightening holes having 45 degree flanges /  |c Paul Kuhn. 
246 3 |a NACA Wartime Reports. Series L. 
264 1 |a Washington, D.C. :  |b National Advisory Committee for Aeronautics,  |c [1942] 
300 |a 1 online resource (12 pages, 13 unnumbered pages 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 Wartime Report / National Advisory Committee for Aeronautics ;  |v number L323 
500 |a NACA Wartime Report L-323. 
500 |a Originally issued as NACA as an Advance Restricted Report (December 1942). 
500 |a Prepared at the Langley Memorial Aeronautical Laboratory, Langley Field, Virginia. 
504 |a Includes bibliographical references. 
520 3 |a Tests were made of 18 shear webs with round lightening holes having 45 degree flanges. The purpose of the tests was to extend the range of a previous investigation to larger ratios of hole diameter to web depth and of web depth to web thickness. Simple empirical formulas are given for the strength and the stiffness of shear webs; these formulas incorporate the results of the previous investigation. Design charts are also given to facilitate the application of the results. 
588 0 |a Print version record. 
590 |a Knovel  |b ACADEMIC - Aerospace & Radar Technology 
650 0 |a Aluminum alloys  |x Testing. 
650 0 |a Holes. 
650 0 |a Strength of materials. 
650 0 |a Flanges. 
650 0 |a Charts, diagrams, etc. 
650 6 |a Trous. 
650 6 |a Résistance des matériaux. 
650 6 |a Tableaux, graphiques, etc. 
650 7 |a strength of materials.  |2 aat 
650 7 |a diagrams.  |2 aat 
650 7 |a Aluminum alloys  |x Testing  |2 fast 
650 7 |a Charts, diagrams, etc.  |2 fast 
650 7 |a Flanges  |2 fast 
650 7 |a Holes  |2 fast 
650 7 |a Strength of materials  |2 fast 
710 1 |a United States.  |b National Advisory Committee for Aeronautics. 
710 2 |a Langley Aeronautical Laboratory. 
776 0 8 |i Print version:  |a Kuhn, Paul.  |t Strength and stiffness of shear webs with round lightening holes having 45 degree flanges  |w (OCoLC)707505373 
830 0 |a Wartime Reports (United States. National Advisory Committee for Aeronautics) ;  |v no. L323. 
856 4 0 |u https://appknovel.uam.elogim.com/kn/resources/kpSSSWRLH4/toc  |z Texto completo 
994 |a 92  |b IZTAP