Handbook of structural stability. Part 2, Buckling of composite elements /
Saved in:
| Main Author | |
|---|---|
| Corporate Author | |
| Format | Electronic eBook |
| Language | English |
| Published |
Washington, D.C. :
National Advisory Committee for Aeronautics,
[1957]
|
| Series | Technical note (United States. National Advisory Committee for Aeronautics) ;
no. 3782. |
| Subjects | |
| Online Access | Full text |
| ISBN | 9781680156270 1680156276 |
| Physical Description | 1 online resource (72 pages) : illustrations |
Cover
| LEADER | 00000cam a2200000 i 4500 | ||
|---|---|---|---|
| 001 | kn-ocn914328453 | ||
| 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 9781680156270 |q (electronic bk.) | ||
| 020 | |a 1680156276 |q (electronic bk.) | ||
| 035 | |a (OCoLC)914328453 |z (OCoLC)951669588 |z (OCoLC)987018204 |z (OCoLC)1316530350 |z (OCoLC)1329355413 |z (OCoLC)1391639797 | ||
| 100 | 1 | |a Becker, Herbert, |d 1918- |1 https://id.oclc.org/worldcat/entity/E39PCjBkyVMVhr9C9DTVXK7Hvd | |
| 245 | 1 | 0 | |a Handbook of structural stability. |n Part 2, |p Buckling of composite elements / |c Herbert Becker. |
| 260 | |a Washington, D.C. : |b National Advisory Committee for Aeronautics, |c [1957] | ||
| 300 | |a 1 online resource (72 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 3782 | |
| 500 | |a NACA TN No. 3782. | ||
| 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 The local buckling of stiffener sections and the buckling of plates with sturdy stiffeners are reviewed, and the results are summarized in charts and tables. Numerical values of buckling coefficients are presented for longitudinally compressed stiffener sections of various shapes, for stiffened plates loaded in longitudinal compression and in shear, and for stiffened cylinders loaded in torsion. Although the data presented consist primarily of elastic-buckling coefficients, the effects of plasticity are discussed for a few special cases. | |
| 590 | |a Knovel |b Knovel (All titles) | ||
| 650 | 0 | |a Structural analysis (Engineering) | |
| 650 | 0 | |a Stability. | |
| 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 | |
| 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. |d Washington, D.C. : National Advisory Committee for Aeronautics, [1957] |w (OCoLC)682897579 |
| 830 | 0 | |a Technical note (United States. National Advisory Committee for Aeronautics) ; |v no. 3782. | |
| 856 | 4 | 0 | |u https://proxy.k.utb.cz/login?url=https://app.knovel.com/hotlink/toc/id:kpHSSPIIB1/handbook-of-structural?kpromoter=marc |y Full text |