Stress and distortion analysis of a swept box beam having bulkheads perpendicular to the spars
Saved in:
| 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. 2232. |
| Subjects | |
| Online Access | Full text |
| ISBN | 9781680156188 1680156187 |
| Physical Description | 1 online resource (90 pages) : illustrations |
Cover
| LEADER | 00000cam a2200000 i 4500 | ||
|---|---|---|---|
| 001 | kn-ocn919130977 | ||
| 003 | OCoLC | ||
| 005 | 20240717213016.0 | ||
| 006 | m o d | ||
| 007 | cr cn||||||||| | ||
| 008 | 150825s1950 dcua obt f000 0 eng d | ||
| 040 | |a KNOVL |b eng |e rda |e pn |c KNOVL |d ZCU |d UAB |d COD |d MERER |d OCLCF |d OCLCQ |d DKU |d CEF |d RRP |d YOU |d S2H |d OCLCO |d TRAAL |d OCLCO |d OCLCQ |d UPM |d OCLCQ |d OCLCO |d OCLCL |d SXB | ||
| 020 | |a 9781680156188 |q (electronic bk.) | ||
| 020 | |a 1680156187 |q (electronic bk.) | ||
| 035 | |a (OCoLC)919130977 | ||
| 100 | 1 | |a Heldenfels, Richard R., |e author. | |
| 245 | 1 | 0 | |a Stress and distortion analysis of a swept box beam having bulkheads perpendicular to the spars / |c by Richard R. Heldenfels, George W. Zender, and Charles Libove. |
| 264 | 1 | |a Washington, D.C. : |b National Advisory Committee for Aeronautics, |c 1950. | |
| 300 | |a 1 online resource (90 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. 2232 | |
| 500 | |a Date of issue: November 1950. | ||
| 500 | |a Report no. NACA-TN-2232 | ||
| 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 method is presented for the approximate calculation of the stresses and distortions in a box beam representing the main structural component of a swept wing with a carry-through section and with bulkheads perpendicular to the spars. The application of the method is illustrated by a numerical example and its results are compared with previously published test data. | |
| 590 | |a Knovel |b Knovel (All titles) | ||
| 650 | 0 | |a Box beams. | |
| 650 | 0 | |a Bulkheads. | |
| 650 | 0 | |a Strains and stresses. | |
| 650 | 0 | |a Structural analysis (Engineering) | |
| 655 | 7 | |a elektronické knihy |7 fd186907 |2 czenas | |
| 655 | 9 | |a electronic books |2 eczenas | |
| 700 | 1 | |a Zender, George W. | |
| 700 | 1 | |a Libove, Charles. | |
| 710 | 1 | |a United States. |b National Advisory Committee for Aeronautics. | |
| 776 | 0 | 8 | |i Print version: |a Heldenfels, Richard R. |t Stress and distortion analysis of a swept box beam having bulkheads perpendicular to the spars |w (OCoLC)664036032 |
| 830 | 0 | |a Technical note (United States. National Advisory Committee for Aeronautics) ; |v no. 2232. | |
| 856 | 4 | 0 | |u https://proxy.k.utb.cz/login?url=https://app.knovel.com/hotlink/toc/id:kpSDASBBHO/stress-and-distortion?kpromoter=marc |y Full text |