Handbook of structural stability. Part 4, Failure of plates and composite elements /
Available theories on failure of flat plates are reviewed, and test data on the postbuckling behavior, effective width, and failure of flat curved plates are correlated.
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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. 3784. |
Subjects: | |
ISBN: | 9781680156294 1680156292 |
Physical Description: | 1 online resource (ii, 93 pages) : illustrations |
LEADER | 03209cam a2200505 i 4500 | ||
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001 | kn-ocn914329610 | ||
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 9781680156294 |q (electronic bk.) | ||
020 | |a 1680156292 |q (electronic bk.) | ||
035 | |a (OCoLC)914329610 |z (OCoLC)951669597 |z (OCoLC)987016667 |z (OCoLC)1315806202 |z (OCoLC)1328436562 |z (OCoLC)1391639799 | ||
100 | 1 | |a Gerard, George. | |
245 | 1 | 0 | |a Handbook of structural stability. |n Part 4, |p Failure of plates and composite elements / |c George Gerard. |
260 | |a Washington, D.C. : |b National Advisory Committee for Aeronautics, |c [1957] | ||
300 | |a 1 online resource (ii, 93 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 3784 | |
500 | |a NACA TN No. 3784. | ||
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 on failure of flat plates are reviewed, and test data on the postbuckling behavior, effective width, and failure of flat curved plates are correlated. | |
520 | 3 | |a Test data on the crippling strength of various formed and extruded shapes are reviewed, from which a generalized method of crippling analysis is formulated. The effects upon the crippling strength of alclad coatings and the increased properties in the corners of formed sections are investigated by use of this analysis. | |
520 | 3 | |a The generalized crippling analysis was applied to a variety of sections and materials in common use. It was found that the crippling strength of all the sections is governed in a simple manner by the developed length-thickness ratio and number of corners of the section. | |
590 | |a Knovel |b Knovel (All titles) | ||
650 | 0 | |a Structural analysis (Engineering) | |
650 | 0 | |a Stability. | |
650 | 0 | |a Plates (Engineering) | |
650 | 0 | |a Columns. | |
650 | 0 | |a Cylinders. | |
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)682899193 |
830 | 0 | |a Technical note (United States. National Advisory Committee for Aeronautics) ; |v no. 3784. | |
856 | 4 | 0 | |u https://proxy.k.utb.cz/login?url=https://app.knovel.com/hotlink/toc/id:kpHSSPIIV5/handbook-of-structural?kpromoter=marc |y Full text |