Critical combinations of shear and longitudinal direct stress for long plates with transverse curvature
Saved in:
| Main Authors | , , |
|---|---|
| Corporate Author | |
| Format | Electronic eBook |
| Language | English |
| Published |
Washington, D.C. :
National Advisory Committee for Aeronautics,
1947.
|
| Series | Technical note (United States. National Advisory Committee for Aeronautics) ;
no. 1347. |
| Subjects | |
| Online Access | Full text |
| ISBN | 9781680156065 1680156063 |
| Physical Description | 1 online resource (27 pages, 9 unnumbered pages) : illustrations, tables |
Cover
| LEADER | 00000cam a2200000 i 4500 | ||
|---|---|---|---|
| 001 | kn-ocn919093316 | ||
| 003 | OCoLC | ||
| 005 | 20240717213016.0 | ||
| 006 | m o d | ||
| 007 | cr cn||||||||| | ||
| 008 | 150824s1947 dcua obt f000 0 eng d | ||
| 040 | |a KNOVL |b eng |e rda |e pn |c KNOVL |d ZCU |d OCLCQ |d UAB |d DKU |d OCLCQ |d CEF |d RRP |d WYU |d YOU |d S2H |d OCLCO |d COP |d OCLCO |d COP |d OCLCO |d OCLCQ |d UPM |d OCLCQ |d OCLCO |d OCLCL |d SXB | ||
| 020 | |a 9781680156065 |q (electronic bk.) | ||
| 020 | |a 1680156063 |q (electronic bk.) | ||
| 035 | |a (OCoLC)919093316 | ||
| 100 | 1 | |a Batdorf, S. B., |e author. | |
| 245 | 1 | 0 | |a Critical combinations of shear and longitudinal direct stress for long plates with transverse curvature / |c by S.B. Batdort, Murry Schildcrout, and Manuel Stein. |
| 264 | 1 | |a Washington, D.C. : |b National Advisory Committee for Aeronautics, |c 1947. | |
| 300 | |a 1 online resource (27 pages, 9 unnumbered pages) : |b illustrations, tables | ||
| 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 technical note ; |v number 1347 | |
| 500 | |a "Langley Memorial Aeronautical Laboratory." | ||
| 500 | |a Date of issue: June 1947. | ||
| 500 | |a Report no. NACA TN No. 1347. | ||
| 504 | |a Includes bibliographical references (pages 23-24) | ||
| 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 theoretical solution is presented for the buckling stresses of long plates with transverse curvature loaded in shear and longitudinal direct stress. The theoretical critical-stress combinations for plates having either simply supported or clamped edges are given in figures and tables and a comparison is made with a previous theoretical solution for simply supported plates. | |
| 590 | |a Knovel |b Knovel (All titles) | ||
| 650 | 0 | |a Plates (Engineering) | |
| 650 | 0 | |a Strains and stresses. | |
| 650 | 0 | |a Buckling (Mechanics) | |
| 650 | 0 | |a Loads (Mechanics) | |
| 650 | 0 | |a Shear (Mechanics) | |
| 655 | 7 | |a elektronické knihy |7 fd186907 |2 czenas | |
| 655 | 9 | |a electronic books |2 eczenas | |
| 700 | 1 | |a Schildcrout, Murry, |e author. | |
| 700 | 1 | |a Stein, Manuel, |e author. | |
| 710 | 1 | |a United States. |b National Advisory Committee for Aeronautics, |e issuing body. | |
| 710 | 2 | |a Langley Aeronautical Laboratory. | |
| 776 | 0 | 8 | |i Print version: |a Batdorf, S.B. |t Critical combinations of shear and longitudinal direct stress for long plates with transverse curvature |w (OCoLC)652540878 |
| 830 | 0 | |a Technical note (United States. National Advisory Committee for Aeronautics) ; |v no. 1347. | |
| 856 | 4 | 0 | |u https://proxy.k.utb.cz/login?url=https://app.knovel.com/hotlink/toc/id:kpCCSLDSL1/critical-combinations-of?kpromoter=marc |y Full text |