The strength of shell bodies-- theory and practice
Saved in:
| Main Author | |
|---|---|
| Corporate Author | |
| Format | Electronic eBook |
| Language | English |
| Published |
Washington, D.C. :
National Advisory Commitee for Aeronautics,
[1937]
|
| Series | Technical memorandum (United States. National Advisory Committee for Aeronautics) ;
no. 838. |
| Subjects | |
| Online Access | Full text |
| ISBN | 9781680156560 168015656X |
| Physical Description | 1 online resource (51 pages, 9 unnumbered pages) : illustrations |
Cover
| LEADER | 00000cam a2200000 i 4500 | ||
|---|---|---|---|
| 001 | kn-ocn919167954 | ||
| 003 | OCoLC | ||
| 005 | 20240717213016.0 | ||
| 006 | m o d | ||
| 007 | cr cn||||||||| | ||
| 008 | 150825s1937 dcua obt f000 0 eng d | ||
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| 020 | |a 9781680156560 |q (electronic bk.) | ||
| 020 | |a 168015656X |q (electronic bk.) | ||
| 035 | |a (OCoLC)919167954 |z (OCoLC)1111582255 |z (OCoLC)1117267102 |z (OCoLC)1229063301 | ||
| 042 | |a dlr | ||
| 100 | 1 | |a Ebner, H., |e author. | |
| 245 | 1 | 4 | |a The strength of shell bodies-- theory and practice / |c H. Ebner. |
| 264 | 1 | |a Washington, D.C. : |b National Advisory Commitee for Aeronautics, |c [1937] | |
| 300 | |a 1 online resource (51 pages, 9 unnumbered 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 Technical memorandums ; |v number 838 | |
| 500 | |a "September 1937." | ||
| 500 | |a NACA TM No. 838. | ||
| 500 | |a Translated from Luftfahrtforschung. Vol. 14, No. 3, March 20, 1937, by the National Advisory Commitee for Aeronautics. | ||
| 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 The monocoque form of airplane construction has introduced a number of new problems to the stress calculator and the designer. The problems for the stress calculator fall into two groups: the determination of the stress condition (shell statics) and the determination of the failing strength (shell strength). The present report summarizes the most important theoretical and experimental results on this subject. | |
| 590 | |a Knovel |b Knovel (All titles) | ||
| 650 | 0 | |a Monocoque construction. | |
| 650 | 0 | |a Shells (Engineering) | |
| 650 | 0 | |a Strains and stresses. | |
| 650 | 0 | |a Mathematics. | |
| 655 | 7 | |a elektronické knihy |7 fd186907 |2 czenas | |
| 655 | 9 | |a electronic books |2 eczenas | |
| 710 | 1 | |a United States. |b National Advisory Commitee for Aeronautics. | |
| 776 | 0 | 8 | |i Print version: |a Ebner, H. |t Strength of shell bodies - theory and practice |w (OCoLC)696399361 |
| 830 | 0 | |a Technical memorandum (United States. National Advisory Committee for Aeronautics) ; |v no. 838. | |
| 856 | 4 | 0 | |u https://proxy.k.utb.cz/login?url=https://app.knovel.com/hotlink/toc/id:kpSSBTPNA1/strength-of-shell?kpromoter=marc |y Full text |