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

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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 Electronic eBook
LanguageEnglish
Published Washington, D.C. : National Advisory Committee for Aeronautics, [1944]
SeriesWartime 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
Online AccessFull text
ISBN9781680156362
1680156365
Physical Description1 online resource (15 pages, 9 unnumbered pages) : illustrations

Cover

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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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