Effect of normal pressure on the critical compressive and shear stress of curved sheet
Saved in:
| Main Author | |
|---|---|
| Corporate Authors | , |
| Other Authors | |
| Format | Electronic eBook |
| Language | English |
| Published |
Washington, D.C. :
National Advisory Committee for Aeronautics,
[1945]
|
| Series | Wartime Reports (United States. National Advisory Committee for Aeronautics) ;
no. L57. |
| Subjects | |
| Online Access | Full text |
| ISBN | 9781680156355 1680156357 |
| Physical Description | 1 online resource (7, [8] pages) : illustrations |
Cover
| LEADER | 00000cam a2200000 i 4500 | ||
|---|---|---|---|
| 001 | kn-ocn914330037 | ||
| 003 | OCoLC | ||
| 005 | 20240717213016.0 | ||
| 006 | m o d | ||
| 007 | cr cn||||||||| | ||
| 008 | 150724s1945 dcua obt f000 0 eng d | ||
| 040 | |a SINTU |b eng |e pn |c SINTU |d SINTU |d OCLCO |d KNOVL |d ZCU |d OCLCQ |d UAB |d DKU |d OCLCF |d OCLCQ |d CEF |d RRP |d YOU |d S2H |d OCLCO |d OCLCQ |d OCLCO |d OCLCQ |d OCLCO |d SXB | ||
| 020 | |a 9781680156355 |q (electronic bk.) | ||
| 020 | |a 1680156357 |q (electronic bk.) | ||
| 035 | |a (OCoLC)914330037 |z (OCoLC)951668476 | ||
| 100 | 1 | |a Rafel, Norman. | |
| 245 | 1 | 0 | |a Effect of normal pressure on the critical compressive and shear stress of curved sheet / |c Norman Rafel and Charles W. Sandlin, Jr. |
| 246 | 3 | |a NACA Wartime Reports. Series L. | |
| 260 | |a Washington, D.C. : |b National Advisory Committee for Aeronautics, |c [1945] | ||
| 300 | |a 1 online resource (7, [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. L57 | |
| 500 | |a NACA Wartime Report L-57. | ||
| 500 | |a Originally issued as NACA as Advance Restricted Report L5B10 (March 1945). | ||
| 500 | |a Prepared at the Langley Memorial Aeronautical Laboratory, Langley Field, Virginia. | ||
| 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 Results are presented of tests of two sets of 20 curved-sheet specimens to determine the effect of normal pressure on the critical compressive and shear stress of curved sheet. It was found that normal pressure raised the critical compressive and shear stress of curved sheet except when outward bulging occurred in compression, in which case the critical stress was lowered by normal pressure. | |
| 590 | |a Knovel |b Knovel (All titles) | ||
| 650 | 0 | |a Box beams. | |
| 650 | 0 | |a Aluminum alloys. | |
| 650 | 0 | |a Plates (Engineering) |x Curvature. | |
| 650 | 0 | |a Loads (Mechanics) | |
| 650 | 0 | |a Shear (Mechanics) | |
| 650 | 0 | |a Buckling (Mechanics) | |
| 650 | 0 | |a Strains and stresses. | |
| 650 | 0 | |a Charts, diagrams, etc. | |
| 655 | 7 | |a elektronické knihy |7 fd186907 |2 czenas | |
| 655 | 9 | |a electronic books |2 eczenas | |
| 700 | 1 | |a Sandlin, Charles W. | |
| 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 and shear stress of curved sheet. |d Washington, D.C. : National Advisory Committee for Aeronautics, [1945] |w (OCoLC)705351009 |
| 830 | 0 | |a Wartime Reports (United States. National Advisory Committee for Aeronautics) ; |v no. L57. | |
| 856 | 4 | 0 | |u https://proxy.k.utb.cz/login?url=https://app.knovel.com/hotlink/toc/id:kpENPCCSS3/effect-of-normal?kpromoter=marc |y Full text |