Critical combinations of torsion and direct axial stress for thin-walled cylinders

A theoretical solution is presented for the determination of the combinations of direct axial stress and torsion which cause thin-walled cylinders with either simply supported or clamped edges to buckle. This theoretical solution is used in conjunction with available test data to develop empirical c...

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Bibliographic Details
Main Author: Batdorf, S. B., (Author)
Corporate Author: Langley Aeronautical Laboratory.
Other Authors: Stein, Manuel., Schildcrout, Murry.
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. 1345.
Subjects:
Shells (Engineering)
Thin-walled structures.
Cylinders.
Strains and stresses.
Torsion.
Buckling (Mechanics)
elektronické knihy
electronic books
ISBN: 9781680156058
1680156055
Physical Description: 1 online resource (28, [8] pages) : illustrations, tables

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Table of contents

LEADER 02986cam a2200505 i 4500
001 kn-ocn914248233
003 OCoLC
005 20240717213016.0
006 m o d
007 cr cn|||||||||
008 150722s1947 dcuad obt f000 0 eng d
040 |a SINTU  |b eng  |e rda  |e pn  |c SINTU  |d SINTU  |d OCLCO  |d SINTU  |d KNOVL  |d ZCU  |d OCLCQ  |d UAB  |d DKU  |d OCLCF  |d OCLCQ  |d CEF  |d RRP  |d UMR  |d MERER  |d WYU  |d OCLCQ  |d YOU  |d OCL  |d S2H  |d OCLCO  |d COP  |d OCLCO  |d COP  |d OCLCO  |d OCLCQ  |d OCLCO  |d OCLCL  |d SXB 
020 |a 9781680156058  |q (electronic bk.) 
020 |a 1680156055  |q (electronic bk.) 
035 |a (OCoLC)914248233  |z (OCoLC)951667856 
100 1 |a Batdorf, S. B.,  |e author. 
245 1 0 |a Critical combinations of torsion and direct axial stress for thin-walled cylinders /  |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 (28, [8] 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. 1345 
500 |a "Langley Memorial Aeronautical Laboratory." 
500 |a Date of issue: June 1947. 
500 |a Report no. NACA TN No. 1345. 
504 |a Includes bibliographical references (page 25) 
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 presented for the determination of the combinations of direct axial stress and torsion which cause thin-walled cylinders with either simply supported or clamped edges to buckle. This theoretical solution is used in conjunction with available test data to develop empirical curves and formulas for use in design. Comparisons are made with theoretical and empirical solutions obtained in other investigations. 
590 |a Knovel  |b Knovel (All titles) 
650 0 |a Shells (Engineering) 
650 0 |a Thin-walled structures. 
650 0 |a Cylinders. 
650 0 |a Strains and stresses. 
650 0 |a Torsion. 
650 0 |a Buckling (Mechanics) 
655 7 |a elektronické knihy  |7 fd186907  |2 czenas 
655 9 |a electronic books  |2 eczenas 
700 1 |a Stein, Manuel. 
700 1 |a Schildcrout, Murry. 
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 combinations of torsion and direct axial stress for thin-walled cylinders.  |d Washington, D.C. : National Advisory Committee for Aeronautics, 1947  |w (OCoLC)652531421 
830 0 |a Technical note (United States. National Advisory Committee for Aeronautics) ;  |v no. 1345. 
856 4 0 |u https://proxy.k.utb.cz/login?url=https://app.knovel.com/hotlink/toc/id:kpCCTDASTT/critical-combinations-of?kpromoter=marc  |y Full text 

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