A Unified theory of plastic buckling of columns and plates

On the basis of modern plasticity considerations, a unified theory of plastic buckling applicable to both columns and plates has been developed. For uniform compression, the theory shows shows that long columns which bend without appreciable twisting require the tangent modulus and that long flanges...

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Bibliographic Details
Main Author: Stowell, Elbridge Z.
Corporate Author: United States. National Advisory Committee for Aeronautics.
Format: eBook
Language: English
Published: Washington, D.C. : National Advisory Committee for Aeronautics, 1948.
Series: Technical note (United States. National Advisory Committee for Aeronautics) ; no. 1556.
Subjects:
ISBN: 9781680156379
1680156373
Physical Description: 1 online resource (31 pages) : illustrations

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Table of contents

LEADER 02612cam a2200433 i 4500
001 kn-ocn914548180
003 OCoLC
005 20240717213016.0
006 m o d
007 cr cn|||||||||
008 150727s1948 dcua obt f000 0 eng d
040 |a SINTU  |b eng  |e pn  |c SINTU  |d SINTU  |d KNOVL  |d ZCU  |d OCLCQ  |d UAB  |d REB  |d DKU  |d OCLCQ  |d CEF  |d RRP  |d YOU  |d S2H  |d OCLCO  |d COP  |d OCLCQ  |d OCLCO  |d OCLCQ  |d OCLCO  |d SXB 
020 |a 9781680156379  |q (electronic bk.) 
020 |a 1680156373  |q (electronic bk.) 
035 |a (OCoLC)914548180  |z (OCoLC)951662098 
100 1 |a Stowell, Elbridge Z. 
245 1 2 |a A Unified theory of plastic buckling of columns and plates /  |c Elbridge Z. Stowell. 
260 |a Washington, D.C. :  |b National Advisory Committee for Aeronautics,  |c 1948. 
300 |a 1 online resource (31 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 technical note ;  |v no. 1556 
500 |a "April 1948." 
500 |a NACA TN No. 1556. 
504 |a Includes bibliographical references. 
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 On the basis of modern plasticity considerations, a unified theory of plastic buckling applicable to both columns and plates has been developed. For uniform compression, the theory shows shows that long columns which bend without appreciable twisting require the tangent modulus and that long flanges which twist without appreciable bending require the secant modulus. Structures that both bend and twist when they buckle require a modulus which is a combination of the secant modulus and the tangent modulus. 
590 |a Knovel  |b Knovel (All titles) 
650 0 |a Columns. 
650 0 |a Plates (Engineering) 
650 0 |a Buckling (Mechanics) 
650 0 |a Mathematical analysis. 
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 Stowell, Elbridge Z.  |t Unified theory of plastic buckling of columns and plates.  |d Washington, D.C. : National Advisory Committee for Aeronautics, 1948  |w (OCoLC)657328900 
830 0 |a Technical note (United States. National Advisory Committee for Aeronautics) ;  |v no. 1556. 
856 4 0 |u https://proxy.k.utb.cz/login?url=https://app.knovel.com/hotlink/toc/id:kpUTPBCPN3/unified-theory-of?kpromoter=marc  |y Full text