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Stress and strain concentration at a circular hole in an infinite plate /

Formulas for stress and strain concentration at a circular hole in an infinite plate under tension have been derived for use in the plastic region. Values of stress concentration obtained from the formula are in good agreement with limited tests on 24S-T3 aluminum-alloy tension panels. The strain co...

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Detalles Bibliográficos
Clasificación:Libro Electrónico
Autor principal: Stowell, Elbridge Z. (Autor)
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, 1950.
Colección:Technical note (United States. National Advisory Committee for Aeronautics) ; no. 2073.
Temas:
Acceso en línea:Texto completo

MARC

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007 cr cnu---unuuu
008 150825s1950 dcua obt f000 0 eng d
040 |a KNOVL  |b eng  |e rda  |e pn  |c KNOVL  |d ZCU  |d UAB  |d DKU  |d OCLCQ  |d CEF  |d RRP  |d YOU  |d S2H  |d OCLCO  |d COP  |d OCLCO  |d OCLCQ  |d UPM  |d OCLCQ  |d OCLCO 
020 |a 9781680156171  |q (electronic bk.) 
020 |a 1680156179  |q (electronic bk.) 
029 1 |a GBVCP  |b 856592196 
035 |a (OCoLC)919130291 
050 4 |a TA660.P6 
082 0 4 |a 624.17765  |2 23 
086 0 |a Y 3.N 21/5:6/2073 
049 |a UAMI 
100 1 |a Stowell, Elbridge Z.,  |e author. 
245 1 0 |a Stress and strain concentration at a circular hole in an infinite plate /  |c Elbridge Z. Stowell. 
264 1 |a Washington, D.C. :  |b National Advisory Committee for Aeronautics,  |c 1950. 
300 |a 1 online resource (14 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 National Advisory Committee for Aeronautics ;  |v number 2073 
500 |a "April 1950." 
500 |a NACA TN No. 2073. 
504 |a Includes bibliographical references. 
520 3 |a Formulas for stress and strain concentration at a circular hole in an infinite plate under tension have been derived for use in the plastic region. Values of stress concentration obtained from the formula are in good agreement with limited tests on 24S-T3 aluminum-alloy tension panels. The strain concentration factor is also in agreement with these tests. 
588 0 |a Print version record. 
590 |a Knovel  |b ACADEMIC - Aerospace & Radar Technology 
650 0 |a Plates (Engineering) 
650 0 |a Holes. 
650 0 |a Strains and stresses. 
650 6 |a Plaques (Ingénierie) 
650 6 |a Trous. 
650 6 |a Contraintes (Mécanique) 
650 7 |a stress.  |2 aat 
650 7 |a strain.  |2 aat 
650 7 |a Holes  |2 fast 
650 7 |a Plates (Engineering)  |2 fast 
650 7 |a Strains and stresses  |2 fast 
710 1 |a United States.  |b National Advisory Committee for Aeronautics. 
730 0 |a Technical Report Archive & Image Library (TRAIL) 
776 0 8 |i Print version:  |a Stowell, Elbridge Z.  |t Stress and strain concentration at a circular hole in an infinite plate  |w (OCoLC)662764206 
830 0 |a Technical note (United States. National Advisory Committee for Aeronautics) ;  |v no. 2073. 
856 4 0 |u https://appknovel.uam.elogim.com/kn/resources/kpSSCCHIP3/toc  |z Texto completo 
994 |a 92  |b IZTAP