Handbook of structural stability. Part VI, Strength of stiffened curved plates and shells /
A comprehensive review of failure of stiffened curved plates and shells is presented.
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Main Author: | |
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Corporate Author: | |
Format: | eBook |
Language: | English |
Published: |
Washington, D.C. :
National Advisory Committee for Aeronautics,
[1958]
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Series: | Technical note (United States. National Advisory Committee for Aeronautics) ;
no. 3786. |
Subjects: | |
ISBN: | 9781680156317 1680156314 |
Physical Description: | 1 online resource (iii, 82 pages) : illustrations |
LEADER | 03054cam a2200493 i 4500 | ||
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001 | kn-ocn919143133 | ||
003 | OCoLC | ||
005 | 20240717213016.0 | ||
006 | m o d | ||
007 | cr cn||||||||| | ||
008 | 150825s1958 dcua obt f000 0 eng d | ||
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020 | |a 9781680156317 |q (electronic bk.) | ||
020 | |a 1680156314 |q (electronic bk.) | ||
035 | |a (OCoLC)919143133 |z (OCoLC)1391639801 | ||
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 |