The effect of internal pressure on the buckling stress of thin-walled circular cylinders under torsion

The results of a series of tests to determine the effect of internal pressure on the buckling load of a thin cylinder under an applied torque indicated that internal pressure raises the shear buckling stress. The experimental results were analyzed with the aid of previously developed theory and a si...

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Bibliographic Details
Main Authors: Crate, Harold, (Author), Batdorf, S. B., (Author), Baab, George W., (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, [1944]
Series: Wartime Reports (United States. National Advisory Committee for Aeronautics) ; no. L67.
Subjects:
Cylinders.
Loads (Mechanics)
Shear (Mechanics)
Buckling (Mechanics)
Strains and stresses.
Charts, diagrams, etc.
elektronické knihy
electronic books
ISBN: 9781680156362
1680156365
Physical Description: 1 online resource (15 pages, 9 unnumbered pages) : illustrations

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Table of contents

LEADER 02890cam a2200517 i 4500
001 kn-ocn919146897
003 OCoLC
005 20240717213016.0
006 m o d
007 cr cn|||||||||
008 150825s1944 dcua obt f000 0 eng d
040 |a KNOVL  |b eng  |e rda  |e pn  |c KNOVL  |d ZCU  |d OCLCQ  |d UAB  |d DKU  |d OCLCQ  |d CEF  |d RRP  |d YOU  |d S2H  |d OCLCO  |d OCLCQ  |d UPM  |d OCLCQ  |d OCLCO  |d OCLCL  |d SXB 
020 |a 9781680156362  |q (electronic bk.) 
020 |a 1680156365  |q (electronic bk.) 
035 |a (OCoLC)919146897 
100 1 |a Crate, Harold,  |e author. 
245 1 4 |a The effect of internal pressure on the buckling stress of thin-walled circular cylinders under torsion /  |c Harold Crate, S.B. Batdorf, and George W. Baab. 
246 3 |a NACA Wartime Reports. Series L. 
264 1 |a Washington, D.C. :  |b National Advisory Committee for Aeronautics,  |c [1944] 
300 |a 1 online resource (15 pages, 9 unnumbered 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 Wartime Report / National Advisory Committee for Aeronautics ;  |v number L67 
500 |a NACA Wartime Report L-67. 
500 |a Originally issued as NACA as Advance Restricted Report L4E27 (May 1944). 
500 |a Prepared at the Langley Memorial Aeronautical Laboratory, Langley Field, Virginia. 
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 The results of a series of tests to determine the effect of internal pressure on the buckling load of a thin cylinder under an applied torque indicated that internal pressure raises the shear buckling stress. The experimental results were analyzed with the aid of previously developed theory and a simple interaction formula was derived. 
504 |a Includes bibliographical references. 
590 |a Knovel  |b Knovel (All titles) 
650 0 |a Cylinders. 
650 0 |a Loads (Mechanics) 
650 0 |a Shear (Mechanics) 
650 0 |a Buckling (Mechanics) 
650 0 |a Strains and stresses. 
650 0 |a Charts, diagrams, etc. 
655 7 |a elektronické knihy  |7 fd186907  |2 czenas 
655 9 |a electronic books  |2 eczenas 
700 1 |a Batdorf, S. B.,  |e author. 
700 1 |a Baab, George W.,  |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 Crate, Harold.  |t Effect of internal pressure on the buckling stress of thin-walled circular cylinders under torsion  |w (OCoLC)705374267 
830 0 |a Wartime Reports (United States. National Advisory Committee for Aeronautics) ;  |v no. L67. 
856 4 0 |u https://proxy.k.utb.cz/login?url=https://app.knovel.com/hotlink/toc/id:kpEIPBSTW3/effect-of-internal?kpromoter=marc  |y Full text 

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