Plastic buckling of simply supported compressed plates

Tests were made of 14S-T6 aluminum-alloy square tubes to determine the critical compressive stress of simply supported flat plates in the plastic range. Excellent agreement is shown with with Stowell's theory for plastic buckling which is based upon a deformation theory of plasticity, close agr...

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Bibliographic Details
Main Authors: Pride, Richard A., (Author), Heimerl, George J., (Author)
Corporate Authors: United States. National Advisory Committee for Aeronautics., Langley Aeronautical Laboratory.
Format: eBook
Language: English
Published: Washington, D.C. : National Advisory Committee for Aeronautics, 1949.
Series: Technical note (United States. National Advisory Committee for Aeronautics) ; no. 1817.
Subjects:
Aluminum alloys.
Tubes.
Deformations (Mechanics)
Buckling (Mechanics)
Plasticity.
Pipe.
elektronické knihy
electronic books
ISBN: 9781680156157
1680156152
Physical Description: 1 online resource (22 pages) : illustrations

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Table of contents

LEADER 02672cam a2200481 i 4500
001 kn-ocn919094657
003 OCoLC
005 20240717213016.0
006 m o d
007 cr cn|||||||||
008 150824s1949 dcua obt f000 0 eng d
040 |a KNOVL  |b eng  |e rda  |e pn  |c KNOVL  |d OCLCF  |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  |d OCLCL  |d SXB 
020 |a 9781680156157  |q (electronic bk.) 
020 |a 1680156152  |q (electronic bk.) 
035 |a (OCoLC)919094657 
100 1 |a Pride, Richard A.,  |e author. 
245 1 0 |a Plastic buckling of simply supported compressed plates /  |c Richard A. Pride and George J. Heimerl. 
264 1 |a Washington, D.C. :  |b National Advisory Committee for Aeronautics,  |c 1949. 
300 |a 1 online resource (22 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 1817 
500 |a Date of issue: April 1949. 
500 |a Report no. NACA-TN-1817. 
504 |a Includes bibliographical references (page 10) 
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 Tests were made of 14S-T6 aluminum-alloy square tubes to determine the critical compressive stress of simply supported flat plates in the plastic range. Excellent agreement is shown with with Stowell's theory for plastic buckling which is based upon a deformation theory of plasticity, close agreement with two other deformation-type theories of plastic buckling and withthe secant-modulus method, and marked disagreement with a buckling theory based upon a flow theory of plasticity. 
590 |a Knovel  |b Knovel (All titles) 
650 0 |a Aluminum alloys. 
650 0 |a Tubes. 
650 0 |a Deformations (Mechanics) 
650 0 |a Buckling (Mechanics) 
650 0 |a Plasticity. 
650 0 |a Pipe. 
655 7 |a elektronické knihy  |7 fd186907  |2 czenas 
655 9 |a electronic books  |2 eczenas 
700 1 |a Heimerl, George J.,  |e author. 
710 1 |a United States.  |b National Advisory Committee for Aeronautics. 
710 2 |a Langley Aeronautical Laboratory. 
776 0 8 |i Print version:  |a Pride, Richard A.  |t Plastic buckling of simply supported compressed plates  |w (OCoLC)659780939 
830 0 |a Technical note (United States. National Advisory Committee for Aeronautics) ;  |v no. 1817. 
856 4 0 |u https://proxy.k.utb.cz/login?url=https://app.knovel.com/hotlink/toc/id:kpPBSSCPN8/plastic-buckling-of?kpromoter=marc  |y Full text 

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