Critical combinations of shear and direct axial stress for curved rectangular panels
Saved in:
| Main Author | |
|---|---|
| Corporate Author | |
| Other Authors | |
| Format | Electronic eBook |
| Language | English |
| Published |
Washington, D.C. :
National Advisory Committee for Aeronautics,
1949.
|
| Series | Technical note (United States. National Advisory Committee for Aeronautics) ;
no. 1928. |
| Subjects | |
| Online Access | Full text |
| ISBN | 9781680156164 1680156160 |
| Physical Description | 1 online resource (29 pages) : illustrations |
Cover
| LEADER | 00000cam a2200000 i 4500 | ||
|---|---|---|---|
| 001 | kn-ocn914328363 | ||
| 003 | OCoLC | ||
| 005 | 20240717213016.0 | ||
| 006 | m o d | ||
| 007 | cr cn||||||||| | ||
| 008 | 150724s1949 ohua obt f000 0 eng d | ||
| 040 | |a SINTU |b eng |e pn |c SINTU |d SINTU |d KNOVL |d ZCU |d OCLCQ |d UAB |d DKU |d OCLCQ |d CEF |d RRP |d WYU |d YOU |d S2H |d OCLCO |d TRAAL |d OCLCQ |d OCLCO |d OCLCQ |d OCLCO |d OCLCL |d SXB | ||
| 020 | |a 9781680156164 |q (electronic bk.) | ||
| 020 | |a 1680156160 |q (electronic bk.) | ||
| 035 | |a (OCoLC)914328363 |z (OCoLC)951667867 | ||
| 100 | 1 | |a Schildcrout, Murry. | |
| 245 | 1 | 0 | |a Critical combinations of shear and direct axial stress for curved rectangular panels / |c Murry Schildcrout and Manuel Stein. |
| 260 | |a Washington, D.C. : |b National Advisory Committee for Aeronautics, |c 1949. | ||
| 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. 1928 | |
| 500 | |a "August 1949." | ||
| 500 | |a NACA TN No. 1928. | ||
| 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 A solution is presented for the problem of the buckling of curved rectangular panels subjected to combinded shear and direct axial stress. Charts giving theoretical critical combinations of shear and direct axial stress are presented for panels having five different length-width ratios. | |
| 520 | 3 | |a Because the actual critical compressive stress of rectangular panels having substantial curvature is known to be much lower than the theoretical value, a semi-empirical method of analysis of curved panels subjected to combined shear and direct axial stress is presented for use in design. | |
| 590 | |a Knovel |b Knovel (All titles) | ||
| 650 | 0 | |a Plates (Engineering) | |
| 650 | 0 | |a Curvature. | |
| 650 | 0 | |a Buckling (Mechanics) | |
| 650 | 0 | |a Shear (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 Stein, Manuel. | |
| 710 | 1 | |a United States. |b National Advisory Committee for Aeronautics. | |
| 776 | 0 | 8 | |i Print version: |a Schildcrout, Murry. |t Critical combinations of shear and direct axial stress for curved rectangular panels. |d Washington, D.C. : National Advisory Committee for Aeronautics, 1949 |w (OCoLC)660169956 |
| 830 | 0 | |a Technical note (United States. National Advisory Committee for Aeronautics) ; |v no. 1928. | |
| 856 | 4 | 0 | |u https://proxy.k.utb.cz/login?url=https://app.knovel.com/hotlink/toc/id:kpCCSDASC1/critical-combinations-of?kpromoter=marc |y Full text |