Handbook of structural stability. Part 3, Buckling of curved plates and shells /
Available theories and test data on buckling of curved plates and shells are reviewed. For torsion and external-pressure loadings, the test data are correlated in terms of linear buckling theories for both the elastic and inelastic ranges.
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Other Authors: | |
Format: | eBook |
Language: | English |
Published: |
Washington, D.C. :
National Advisory Committee for Aeronautics,
[1957]
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Series: | Technical note (United States. National Advisory Committee for Aeronautics) ;
no. 3783. |
Subjects: | |
ISBN: | 9781680156287 1680156284 |
Physical Description: | 1 online resource (iii, 154 pages) : illustrations |
LEADER | 03273cam a2200493 i 4500 | ||
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001 | kn-ocn914328598 | ||
003 | OCoLC | ||
005 | 20240717213016.0 | ||
006 | m o d | ||
007 | cr cn||||||||| | ||
008 | 150724s1957 dcua obt f000 0 eng d | ||
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020 | |a 9781680156287 |q (electronic bk.) | ||
020 | |a 1680156284 |q (electronic bk.) | ||
035 | |a (OCoLC)914328598 |z (OCoLC)951669596 |z (OCoLC)987019282 |z (OCoLC)1315955853 |z (OCoLC)1328928948 |z (OCoLC)1391639798 | ||
100 | 1 | |a Gerard, George. | |
245 | 1 | 0 | |a Handbook of structural stability. |n Part 3, |p Buckling of curved plates and shells / |c George Gerard and Herbert Becker. |
260 | |a Washington, D.C. : |b National Advisory Committee for Aeronautics, |c [1957] | ||
300 | |a 1 online resource (iii, 154 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 3783 | |
500 | |a NACA TN No. 3783. | ||
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 Available theories and test data on buckling of curved plates and shells are reviewed. For torsion and external-pressure loadings, the test data are correlated in terms of linear buckling theories for both the elastic and inelastic ranges. | |
520 | 3 | |a The cases which exhibit a marked disagreement between linear theory and test data include those of curved plates and cylinders under axial compression, cylinders under bending, and spherical plates under external pressure. These cases have been analyzed by a unified semiempirical approach for both the elastic and inelastic ranges which is satisfactory for analysis and design purposes. | |
520 | 3 | |a The effects of internal pressure on buckling of elements under uniaxial loads are discussed and data on various combined loadings are presented in interaction form. | |
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 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 Becker, Herbert, |d 1918- |1 https://id.oclc.org/worldcat/entity/E39PCjBkyVMVhr9C9DTVXK7Hvd | |
710 | 1 | |a United States. |b National Advisory Committee for Aeronautics. | |
776 | 0 | 8 | |i Print version: |a Gerard, George. |t Handbook of structural stability. |d Washington, D.C. : National Advisory Committee for Aeronautics, [1957] |w (OCoLC)682898018 |
830 | 0 | |a Technical note (United States. National Advisory Committee for Aeronautics) ; |v no. 3783. | |
856 | 4 | 0 | |u https://proxy.k.utb.cz/login?url=https://app.knovel.com/hotlink/toc/id:kpHSSPIII5/handbook-of-structural?kpromoter=marc |y Full text |