Compressive buckling of simply supported curved plates and cylinders of sandwich construction

Theoretical solutions are presented for the buckling in uniform axial compression of two types of simply supported curved sandwich plates: the corrugated-core type and the isotropic type. Results are given in the form of equations and curves.

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Bibliographic Details
Main Author: Stein, Manuel.
Corporate Author: United States. National Advisory Committee for Aeronautics.
Other Authors: Mayers, J.
Format: eBook
Language: English
Published: Washington, D.C. : National Advisory Committee for Aeronautics, 1952.
Series: Technical note (United States. National Advisory Committee for Aeronautics) ; no. 2601.
Subjects:
Plates (Engineering) > Curvature.
Cylinders.
Sandwich construction.
Buckling (Mechanics)
Loads (Mechanics)
Strains and stresses.
elektronické knihy
electronic books
ISBN: 9781680156232
1680156233
Physical Description: 1 online resource (34 pages) : illustrations

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Table of contents

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001 kn-ocn914328448
003 OCoLC
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006 m o d
007 cr cn|||||||||
008 150724s1952 ohua obt f000 0 eng d
040 |a SINTU  |b eng  |e pn  |c 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 OCLCQ  |d OCLCO  |d TRAAL  |d OCLCQ  |d OCLCO  |d OCLCL  |d SXB 
020 |a 9781680156232  |q (electronic bk.) 
020 |a 1680156233  |q (electronic bk.) 
035 |a (OCoLC)914328448  |z (OCoLC)951667414 
100 1 |a Stein, Manuel. 
245 1 0 |a Compressive buckling of simply supported curved plates and cylinders of sandwich construction /  |c Manuel Stein and J. Mayers. 
260 |a Washington, D.C. :  |b National Advisory Committee for Aeronautics,  |c 1952. 
300 |a 1 online resource (34 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. 2601 
500 |a "January 1952." 
500 |a NACA TN No. 2601. 
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 Theoretical solutions are presented for the buckling in uniform axial compression of two types of simply supported curved sandwich plates: the corrugated-core type and the isotropic type. Results are given in the form of equations and curves. 
590 |a Knovel  |b Knovel (All titles) 
650 0 |a Plates (Engineering)  |x Curvature. 
650 0 |a Cylinders. 
650 0 |a Sandwich construction. 
650 0 |a Buckling (Mechanics) 
650 0 |a Loads (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 Mayers, J. 
710 1 |a United States.  |b National Advisory Committee for Aeronautics. 
776 0 8 |i Print version:  |a Stein, Manuel.  |t Compressive buckling of simply supported curved plates and cylinders of sandwich construction.  |d Washington, D.C. : National Advisory Committee for Aeronautics, 1952  |w (OCoLC)666432975 
830 0 |a Technical note (United States. National Advisory Committee for Aeronautics) ;  |v no. 2601. 
856 4 0 |u https://proxy.k.utb.cz/login?url=https://app.knovel.com/hotlink/toc/id:kpCBSSCPC5/compressive-buckling-of?kpromoter=marc  |y Full text 

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