Buckling of thin-walled cylinder under axial compression and internal pressure

An investigation was made of a thin-walled cylinder under axial compression and various internal pressures to study the effect of the internal pressure on the compressive buckling stress of the cylinder. A theoretical analysis based on a large-deflection theory was also made. The theoretically predi...

Full description

Saved in:
Bibliographic Details
Main Author: Lo, Hsu.
Corporate Author: United States. National Advisory Committee for Aeronautics.
Other Authors: Crate, Harold., Schwartz, Edward B.
Format: eBook
Language: English
Published: Washington, D.C. : National Advisory Committee for Aeronautics, 1950.
Series: Technical note (United States. National Advisory Committee for Aeronautics) ; no. 2021.
Subjects:
Thin-walled structures.
Cylinders.
Buckling (Mechanics)
Strains and stresses.
elektronické knihy
electronic books
ISBN: 9781680156195
1680156195
Physical Description: 1 online resource (29 pages) : illustrations

Cover

Table of contents

LEADER 02524cam a2200469 a 4500
001 kn-ocn885198337
003 OCoLC
005 20240717213016.0
006 m o d
007 cr cn|||||||||
008 140801e195001 ohua obt f000 0 eng d
040 |a OCLCE  |b eng  |e pn  |c OCLCE  |d KNOVL  |d ZCU  |d OCLCQ  |d UAB  |d DKU  |d OCLCQ  |d CEF  |d RRP  |d YOU  |d S2H  |d OCLCO  |d OCLCQ  |d COP  |d OCLCO  |d OCLCQ  |d OCLCO  |d SXB 
020 |a 9781680156195  |q (electronic bk.) 
020 |a 1680156195  |q (electronic bk.) 
035 |a (OCoLC)885198337  |z (OCoLC)951666777  |z (OCoLC)977239162  |z (OCoLC)987676097  |z (OCoLC)1047743184 
042 |a dlr 
100 1 |a Lo, Hsu. 
245 1 0 |a Buckling of thin-walled cylinder under axial compression and internal pressure /  |c Hsu Lo, Harold Crate, and Edward B. Schwartz. 
260 |a Washington, D.C. :  |b National Advisory Committee for Aeronautics,  |c 1950. 
300 |a 1 online resource (29 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 no. 2021 
500 |a "January 1950." 
500 |a NACA TN No. 2021. 
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 An investigation was made of a thin-walled cylinder under axial compression and various internal pressures to study the effect of the internal pressure on the compressive buckling stress of the cylinder. A theoretical analysis based on a large-deflection theory was also made. The theoretically predicted increase of compressive buckling stress due to internal pressure agrees fairly well with the experimental results. 
590 |a Knovel  |b Knovel (All titles) 
650 0 |a Thin-walled structures. 
650 0 |a Cylinders. 
650 0 |a Buckling (Mechanics) 
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 Crate, Harold. 
700 1 |a Schwartz, Edward B. 
710 1 |a United States.  |b National Advisory Committee for Aeronautics. 
776 0 8 |i Print version:  |w (OCoLC)662520567 
830 0 |a Technical note (United States. National Advisory Committee for Aeronautics) ;  |v no. 2021. 
856 4 0 |u https://proxy.k.utb.cz/login?url=https://app.knovel.com/hotlink/toc/id:kpBTWCUACR/buckling-of-thin?kpromoter=marc  |y Full text 

Similar Items