Critical-stress of thin-walled cylinders in axial compression

Empirical design curves are presented for the critical stress of thin-walled cylinders loaded in axial compression. These curves are plotted in terms of nondimensional parameters of small-deflection theory and are compared with theoretical curves derived for the buckling of cylinders with simply sup...

Full description

Saved in:
Bibliographic Details
Main Authors: Batdorf, S. B., (Author), Schildcrout, Murry, (Author), Stein, Manuel, (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, 1947.
Series: Technical note (United States. National Advisory Committee for Aeronautics) ; 1343.
Subjects:
Thin-walled structures.
Cylinders.
Strains and stresses.
elektronické knihy
electronic books
ISBN: 9781680156119
168015611X
Physical Description: 1 online resource (17 pages) : illustrations

Cover

Table of contents

LEADER 03002cam a2200469 i 4500
001 kn-ocn919093987
003 OCoLC
005 20240717213016.0
006 m o d
007 cr cn|||||||||
008 150824s1947 dcua ob f000 0 eng d
040 |a KNOVL  |b eng  |e rda  |e pn  |c KNOVL  |d KNOVL  |d ZCU  |d UAB  |d OCL  |d DKU  |d OCLCQ  |d CEF  |d RRP  |d WYU  |d YOU  |d S2H  |d OCLCO  |d COP  |d OCLCO  |d OCLCQ  |d UPM  |d OCLCQ  |d OCLCO  |d OCLCL  |d SXB 
020 |a 9781680156119  |q (electronic bk.) 
020 |a 168015611X  |q (electronic bk.) 
035 |a (OCoLC)919093987 
100 1 |a Batdorf, S. B.,  |e author. 
245 1 0 |a Critical-stress of thin-walled cylinders in axial compression /  |c by S.B. Batdorf, Murry Schildcrout, and Manuel Stein, Langley Memorial Aeronautical Laboratory, Langley Field, Va. 
264 1 |a Washington, D.C. :  |b National Advisory Committee for Aeronautics,  |c 1947. 
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 Technical note ;  |v no. 1343 
500 |a "Langley Memorial Aeronautical Laboratory." 
500 |a Date of issue: June 1947. 
500 |a Report no. NACA-TN-1343. 
504 |a Includes bibliographical references (pages 15-16) 
506 |a Plný text je dostupný pouze z IP adres počítačů Univerzity Tomáše Bati ve Zlíně nebo vzdáleným přístupem pro zaměstnance a studenty 
520 |a Empirical design curves are presented for the critical stress of thin-walled cylinders loaded in axial compression. These curves are plotted in terms of nondimensional parameters of small-deflection theory and are compared with theoretical curves derived for the buckling of cylinders with simply supported and clamped edges. An empirical equation is given for the buckling of cylinders having a length-radius ratio greater than about 0.75. The test data obtained from various sources follow the general trend of the theoretical curve for cylinders with clamped edges, agreeing closely with the theory in the case of short cylinders, but falling considerably below the theoretical results for long cylinders. --  |c Provided by publisher. 
590 |a Knovel  |b Knovel (All titles) 
650 0 |a Thin-walled structures. 
650 0 |a Cylinders. 
650 0 |a Strains and stresses. 
655 7 |a elektronické knihy  |7 fd186907  |2 czenas 
655 9 |a electronic books  |2 eczenas 
700 1 |a Schildcrout, Murry,  |e author. 
700 1 |a Stein, Manuel,  |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 Batdorf, S.B.  |t Critical-stress of thin-walled cylinders in axial compression  |w (OCoLC)904438253 
830 0 |a Technical note (United States. National Advisory Committee for Aeronautics) ;  |v 1343. 
856 4 0 |u https://proxy.k.utb.cz/login?url=https://app.knovel.com/hotlink/toc/id:kpCSTWCACB/critical-stress-of?kpromoter=marc  |y Full text 

Similar Items