Effect of normal pressure on the critical compressive stress of curved sheet
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| Main Author | |
|---|---|
| Corporate Authors | , |
| Format | Electronic eBook |
| Language | English |
| Published |
Washington, D.C. :
National Advisory Committee for Aeronautics,
[1942]
|
| Series | Wartime Reports (United States. National Advisory Committee for Aeronautics) ;
no. L258. |
| Subjects | |
| Online Access | Full text |
| ISBN | 9781680156348 1680156349 |
| Physical Description | 1 online resource (2, [8] pages) : illustrations |
Cover
| LEADER | 00000cam a2200000 i 4500 | ||
|---|---|---|---|
| 001 | kn-ocn914330185 | ||
| 003 | OCoLC | ||
| 005 | 20240717213016.0 | ||
| 006 | m o d | ||
| 007 | cr cn||||||||| | ||
| 008 | 150724s1942 dcua ot f000 0 eng d | ||
| 040 | |a SINTU |b eng |e pn |c SINTU |d KNOVL |d ZCU |d OCLCQ |d UAB |d DKU |d OCLCQ |d CEF |d RRP |d YOU |d S2H |d OCLCO |d OCLCQ |d OCLCO |d OCLCQ |d OCLCO |d SXB | ||
| 020 | |a 9781680156348 |q (electronic bk.) | ||
| 020 | |a 1680156349 |q (electronic bk.) | ||
| 035 | |a (OCoLC)914330185 |z (OCoLC)951667782 | ||
| 100 | 1 | |a Rafel, Norman. | |
| 245 | 1 | 0 | |a Effect of normal pressure on the critical compressive stress of curved sheet / |c Norman Rafel. |
| 246 | 3 | |a NACA Wartime Reports. Series L. | |
| 260 | |a Washington, D.C. : |b National Advisory Committee for Aeronautics, |c [1942] | ||
| 300 | |a 1 online resource (2, [8] 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 Wartime Report / National Advisory Committee for Aeronautics ; |v no. L258 | |
| 500 | |a NACA Wartime Report L-258. | ||
| 500 | |a Originally issued as NACA as a Restricted Bulletin (November 1942). | ||
| 500 | |a Prepared at the Langley Memorial Aeronautical Laboratory, Langley Field, Virginia. | ||
| 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 Results are presented of tests of two specimens tested to study the effect of normal pressure on the critical compressive stress for thin curved sheets. These specimens are designated by their respective rib spacings of 10 inches and 30 inches. The relationship between compressive stress and normal pressure at which buckles disappeared is independent of whether the buckles were made to disappear by increase of normal pressure or decrease of compressive stress. | |
| 590 | |a Knovel |b Knovel (All titles) | ||
| 650 | 0 | |a Atmospheric pressure. | |
| 650 | 0 | |a Buckling (Mechanics) | |
| 650 | 0 | |a Strains and stresses. | |
| 650 | 0 | |a Loads (Mechanics) | |
| 650 | 0 | |a Charts, diagrams, etc. | |
| 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. | |
| 710 | 2 | |a Langley Aeronautical Laboratory. | |
| 776 | 0 | 8 | |i Print version: |a Rafel, Norman. |t Effect of normal pressure on the critical compressive stress of curved sheet. |d Washington, D.C. : National Advisory Committee for Aeronautics, [1942] |w (OCoLC)707099582 |
| 830 | 0 | |a Wartime Reports (United States. National Advisory Committee for Aeronautics) ; |v no. L258. | |
| 856 | 4 | 0 | |u https://proxy.k.utb.cz/login?url=https://app.knovel.com/hotlink/toc/id:kpENPCCSC1/effect-of-normal?kpromoter=marc |y Full text |