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

Saved in:
Bibliographic Details
Main Author Stein, Manuel
Corporate Author United States. National Advisory Committee for Aeronautics
Other Authors Mayers, J.
Format Electronic eBook
LanguageEnglish
Published Washington, D.C. : National Advisory Committee for Aeronautics, 1952.
SeriesTechnical 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
Online AccessFull text
ISBN9781680156232
1680156233
Physical Description1 online resource (34 pages) : illustrations

Cover

LEADER 00000cam a2200000 i 4500
001 kn-ocn914328448
003 OCoLC
005 20240717213016.0
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 

Similar Items