Buckling of thin-walled cylinder under axial compression and internal pressure
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| Main Author | |
|---|---|
| Corporate Author | |
| Other Authors | , |
| Format | Electronic eBook |
| Language | English |
| Published |
Washington, D.C. :
National Advisory Committee for Aeronautics,
1950.
|
| Series | Technical note (United States. National Advisory Committee for Aeronautics) ;
no. 2021. |
| Subjects | |
| Online Access | Full text |
| ISBN | 9781680156195 1680156195 |
| Physical Description | 1 online resource (29 pages) : illustrations |
Cover
| LEADER | 00000cam a2200000 a 4500 | ||
|---|---|---|---|
| 001 | kn-ocn885198337 | ||
| 003 | OCoLC | ||
| 005 | 20240717213016.0 | ||
| 006 | m o d | ||
| 007 | cr cn||||||||| | ||
| 008 | 140801e195001 ohua obt f000 0 eng d | ||
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| 020 | |a 9781680156195 |q (electronic bk.) | ||
| 020 | |a 1680156195 |q (electronic bk.) | ||
| 035 | |a (OCoLC)885198337 |z (OCoLC)951666777 |z (OCoLC)977239162 |z (OCoLC)987676097 |z (OCoLC)1047743184 | ||
| 042 | |a dlr | ||
| 100 | 1 | |a Lo, Hsu. | |
| 245 | 1 | 0 | |a Buckling of thin-walled cylinder under axial compression and internal pressure / |c Hsu Lo, Harold Crate, and Edward B. Schwartz. |
| 260 | |a Washington, D.C. : |b National Advisory Committee for Aeronautics, |c 1950. | ||
| 300 | |a 1 online resource (29 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 National Advisory Committee for Aeronautics ; |v no. 2021 | |
| 500 | |a "January 1950." | ||
| 500 | |a NACA TN No. 2021. | ||
| 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 An investigation was made of a thin-walled cylinder under axial compression and various internal pressures to study the effect of the internal pressure on the compressive buckling stress of the cylinder. A theoretical analysis based on a large-deflection theory was also made. The theoretically predicted increase of compressive buckling stress due to internal pressure agrees fairly well with the experimental results. | |
| 590 | |a Knovel |b Knovel (All titles) | ||
| 650 | 0 | |a Thin-walled structures. | |
| 650 | 0 | |a Cylinders. | |
| 650 | 0 | |a Buckling (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 Crate, Harold. | |
| 700 | 1 | |a Schwartz, Edward B. | |
| 710 | 1 | |a United States. |b National Advisory Committee for Aeronautics. | |
| 776 | 0 | 8 | |i Print version: |w (OCoLC)662520567 |
| 830 | 0 | |a Technical note (United States. National Advisory Committee for Aeronautics) ; |v no. 2021. | |
| 856 | 4 | 0 | |u https://proxy.k.utb.cz/login?url=https://app.knovel.com/hotlink/toc/id:kpBTWCUACR/buckling-of-thin?kpromoter=marc |y Full text |