Handbook of structural stability. Part VI, Strength of stiffened curved plates and shells /

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Bibliographic Details
Main Author Becker, Herbert, 1918- (Author)
Corporate Author United States. National Advisory Committee for Aeronautics
Format Electronic eBook
LanguageEnglish
Published Washington, D.C. : National Advisory Committee for Aeronautics, [1958]
SeriesTechnical note (United States. National Advisory Committee for Aeronautics) ; no. 3786.
Subjects
Online AccessFull text
ISBN9781680156317
1680156314
Physical Description1 online resource (iii, 82 pages) : illustrations

Cover

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100 1 |a Becker, Herbert,  |d 1918-  |e author.  |1 https://id.oclc.org/worldcat/entity/E39PCjBkyVMVhr9C9DTVXK7Hvd 
245 1 0 |a Handbook of structural stability.  |n Part VI,  |p Strength of stiffened curved plates and shells /  |c Herbert Becker. 
264 1 |a Washington, D.C. :  |b National Advisory Committee for Aeronautics,  |c [1958] 
300 |a 1 online resource (iii, 82 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 Technical note / National Advisory Committee for Aeronautics ;  |v 3786 
500 |a NACA TN No. 3786. 
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 A comprehensive review of failure of stiffened curved plates and shells is presented. 
520 3 |a Panel instability in stiffened curved plates and general instability of stiffened cylinders are discussed. The loadings considered for the plates are axial, shear, and the combination of the two. For the cylinders, bending, external pressure, torsion, transverse shear, and combinations of these loads are considered. 
520 3 |a General instability in stiffened cylinders was investigated. For bending and torsion loads, test data and theory were correlated. For external pressure several existing theories were compared. As a result of this investigation a unified theoretical approach to analysis of general instability in stiffened cylinders was developed. 
590 |a Knovel  |b Knovel (All titles) 
650 0 |a Structural analysis (Engineering) 
650 0 |a Stability. 
650 0 |a Plates (Engineering)  |x Curvature. 
650 0 |a Shells (Engineering)  |x Curvature. 
650 0 |a Strength of materials. 
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 
710 1 |a United States.  |b National Advisory Committee for Aeronautics. 
776 0 8 |i Print version:  |a Becker, Herbert.  |t Handbook of structural stability  |w (OCoLC)682898406 
830 0 |a Technical note (United States. National Advisory Committee for Aeronautics) ;  |v no. 3786. 
856 4 0 |u https://proxy.k.utb.cz/login?url=https://app.knovel.com/hotlink/toc/id:kpHSSPVIS1/handbook-of-structural?kpromoter=marc  |y Full text