Experimental investigation of the effects of plastic flow in a tension panel with a circular hole

Seven uniformly dimensioned 24S-T tension panels with a central circular hole were subjected to various loads in order to study the effects of plastic flow at the point of maximum stress concentration. The results, presented in graphical form, show that, as the amount of plastic flow increases, the...

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Bibliographic Details
Main Author: Griffith, George E., (Author)
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. 1705.
Subjects:
Aluminum alloys.
Plates (Engineering)
Holes.
Loads (Mechanics)
Alloys > Creep.
Strains and stresses.
elektronické knihy
electronic books
ISBN: 9781680156140
1680156144
Physical Description: 1 online resource (17 pages) : illustrations

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Table of contents

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001 kn-ocn919094518
003 OCoLC
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006 m o d
007 cr cn|||||||||
008 150824s1948 dcua obt f000 0 eng d
040 |a KNOVL  |b eng  |e rda  |e pn  |c KNOVL  |d ZCU  |d UAB  |d DKU  |d OCLCF  |d OCLCQ  |d CEF  |d RRP  |d WYU  |d YOU  |d S2H  |d OCLCO  |d TRAAL  |d OCLCO  |d OCLCQ  |d UPM  |d OCLCQ  |d OCLCO  |d OCLCL  |d SXB 
020 |a 9781680156140  |q (electronic bk.) 
020 |a 1680156144  |q (electronic bk.) 
035 |a (OCoLC)919094518 
100 1 |a Griffith, George E.,  |e author. 
245 1 0 |a Experimental investigation of the effects of plastic flow in a tension panel with a circular hole /  |c by George E. Griffith. 
264 1 |a Washington, D.C. :  |b National Advisory Committee for Aeronautics,  |c 1948. 
300 |a 1 online resource (17 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 number 1705 
500 |a "September 1948." 
500 |a NACA TN No. 1705. 
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 Seven uniformly dimensioned 24S-T tension panels with a central circular hole were subjected to various loads in order to study the effects of plastic flow at the point of maximum stress concentration. The results, presented in graphical form, show that, as the amount of plastic flow increases, the stress concentration factor is appreciably reduced and the strain concentration factor is appreciably increased. Subjecting the panels to 100 repeated loading cycles caused no change to occur in the maximum values of the stress and strain concentration factors. 
590 |a Knovel  |b Knovel (All titles) 
650 0 |a Aluminum alloys. 
650 0 |a Plates (Engineering) 
650 0 |a Holes. 
650 0 |a Loads (Mechanics) 
650 0 |a Alloys  |x Creep. 
650 0 |a Strains and stresses. 
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 Griffith, George E.  |t Experimental investigation of the effects of plastic flow in a tension panel with a circular hole  |w (OCoLC)658230735 
830 0 |a Technical note (United States. National Advisory Committee for Aeronautics) ;  |v no. 1705. 
856 4 0 |u https://proxy.k.utb.cz/login?url=https://app.knovel.com/hotlink/toc/id:kpEIEPFTP3/experimental-investigation-of?kpromoter=marc  |y Full text 

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