Critical stress of thin-walled cylinders in torsion

A theoretical solution is given of the critical stress of thin-walled cylinders loaded in torsion. The results are presented in terms of a few simple formulas and curves which are applicable to a wide range of cylinder dimensions from very short cylinders of large radius to long cylinders of small r...

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Bibliographic Details
Main Authors: Batdorf, S. B., (Author), Stein, Manuel, (Author), Schildcrout, Murry, (Author)
Corporate Author: 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) ; no. 1344.
Subjects:
Shells (Engineering) > Thin-walled structures.
Cylinders.
Strains and stresses.
Torsion.
elektronické knihy
electronic books
ISBN: 9781680156041
1680156047
Physical Description: 1 online resource (21, [5] pages) : illustrations, tables

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003 OCoLC
005 20240717213016.0
006 m o d
007 cr cn|||||||||
008 150719e194706 dcuad obt f000 0 eng d
040 |a SINTU  |b eng  |e rda  |e pn  |c SINTU  |d SINTU  |d OCLCO  |d KNOVL  |d ZCU  |d OCLCQ  |d UAB  |d DKU  |d OCLCF  |d OCLCQ  |d CEF  |d RRP  |d WYU  |d YOU  |d S2H  |d OCLCO  |d COP  |d OCLCO  |d COP  |d OCLCO  |d OCLCQ  |d UPM  |d OCLCQ  |d OCLCO  |d OCLCL  |d SXB 
020 |a 9781680156041  |q (electronic bk.) 
020 |a 1680156047  |q (electronic bk.) 
035 |a (OCoLC)914158513  |z (OCoLC)951667875 
100 1 |a Batdorf, S. B.,  |e author. 
245 1 0 |a Critical stress of thin-walled cylinders in torsion /  |c by S.B. Batdort, Manuel Stein and Murry Schildcrout. 
264 1 |a Washington, D.C. :  |b National Advisory Committee for Aeronautics,  |c 1947. 
300 |a 1 online resource (21, [5] pages) :  |b illustrations, tables 
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 no. 1344 
500 |a "Langley Memorial Aeronautical Laboratory." 
500 |a Date of issue: June 1947. 
500 |a Report no. NACA TN No. 1344. 
504 |a Includes bibliographical references (page 19) 
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 A theoretical solution is given of the critical stress of thin-walled cylinders loaded in torsion. The results are presented in terms of a few simple formulas and curves which are applicable to a wide range of cylinder dimensions from very short cylinders of large radius to long cylinders of small radius. Theoretical results are found to be in somewhat better agreement with experimental results than previous theoretical work for the same range of cylinder dimensions. 
590 |a Knovel  |b Knovel (All titles) 
650 0 |a Shells (Engineering)  |x Thin-walled structures. 
650 0 |a Cylinders. 
650 0 |a Strains and stresses. 
650 0 |a Torsion. 
655 7 |a elektronické knihy  |7 fd186907  |2 czenas 
655 9 |a electronic books  |2 eczenas 
700 1 |a Stein, Manuel,  |e author. 
700 1 |a Schildcrout, Murry,  |e author. 
710 1 |a United States.  |b National Advisory Committee for Aeronautics,  |e issuing body. 
710 2 |a Langley Aeronautical Laboratory. 
776 0 8 |i Print version:  |a Batdorf, S.B.  |t Critical stress of thin-walled cylinders in torsion.  |d Washington, D.C. : National Advisory Committee for Aeronautics, 1947  |w (OCoLC)652531296 
830 0 |a Technical note (United States. National Advisory Committee for Aeronautics) ;  |v no. 1344. 
856 4 0 |u https://proxy.k.utb.cz/login?url=https://app.knovel.com/hotlink/toc/id:kpCSTWCTN7/critical-stress-of?kpromoter=marc  |y Full text 

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