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Stresses around rectangular cut-outs in skin-stringer panels under axial loads - II /
Cut-outs in wings or fuselages produce stress concentrations that present a serious problem to the stress analyst. As a partial solution of the general problem, this paper presents formulas for calculating the stress distribution around rectangular cut-outs in axially loaded panels. The formulas are...
| Clasificación: | Libro Electrónico |
|---|---|
| Autor principal: | |
| Autores Corporativos: | , |
| Otros Autores: | , |
| Formato: | Electrónico eBook |
| Idioma: | Inglés |
| Publicado: |
Langley Field, VA :
Langley Memorial Aeronautical Laboratory,
1943.
|
| Colección: | NACA WR ;
L-368 |
| Temas: | |
| Acceso en línea: | Texto completo |
MARC
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| 001 | KNOVEL_ocn857368754 | ||
| 003 | OCoLC | ||
| 005 | 20231027140348.0 | ||
| 006 | m o d | ||
| 007 | cr bn||||||abp | ||
| 007 | cr bn||||||ada | ||
| 008 | 130901e194310 vauado obt f000 0 eng d | ||
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| 019 | |a 951660439 |a 977856136 |a 987733981 |a 1047754267 |a 1229061830 | ||
| 020 | |a 9781680156485 |q (electronic bk.) | ||
| 020 | |a 1680156489 |q (electronic bk.) | ||
| 029 | 1 | |a GBVCP |b 85659069X | |
| 035 | |a (OCoLC)857368754 |z (OCoLC)951660439 |z (OCoLC)977856136 |z (OCoLC)987733981 |z (OCoLC)1047754267 |z (OCoLC)1229061830 | ||
| 042 | |a dlr | ||
| 050 | 4 | |a TA404.8 | |
| 082 | 0 | 4 | |a 620.11292 |2 23 |
| 049 | |a UAMI | ||
| 100 | 1 | |a Kuhn, Paul. | |
| 245 | 1 | 0 | |a Stresses around rectangular cut-outs in skin-stringer panels under axial loads - II / |c by Paul Kuhn, John E. Duberg, and Simon H. Diskin. |
| 246 | 3 | |a NACA wartime reports | |
| 260 | |a Langley Field, VA : |b Langley Memorial Aeronautical Laboratory, |c 1943. | ||
| 300 | |a 1 online resource (46 pages, [32] leaves) : |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 NACA WR ; |v L-368 | |
| 500 | |a "Originally issued October 1943 as Advance Restricted Report 3J02." | ||
| 500 | |a "NACA WARTIME REPORTS are reprints of papers originally issued to provide rapid distribution of advance research results to an authorized group requiring them for the war effort. They were previously held under a security status but are now unclassified. Some of these reports were not technically edited. All have been reproduced without change in order to expedite general distribution." | ||
| 504 | |a Includes bibliographical references (page 44). | ||
| 520 | |a Cut-outs in wings or fuselages produce stress concentrations that present a serious problem to the stress analyst. As a partial solution of the general problem, this paper presents formulas for calculating the stress distribution around rectangular cut-outs in axially loaded panels. The formulas are derived by means of the substitute-stringer method of shear-lag analysis. In a previous paper published under the same title as the present one, the analysis had been based on a substitute structure containing only two stringers. The present solution is based on a substitute structure containing three stringers and is more complete as well as more accurate than the previous one. It was found that the results could be used to improve the accuracy of the previous solution without appreciably reducing the speed of calculation. Details are given of the three-stringer solution as well as of the modified two-stringer solution. | ||
| 506 | |3 Use copy |f Restrictions unspecified |2 star |5 MiAaHDL | ||
| 533 | |a Electronic reproduction. |b [Place of publication not identified] : |c HathiTrust Digital Library, |d 2013. |5 MiAaHDL | ||
| 538 | |a Master and use copy. Digital master created according to Benchmark for Faithful Digital Reproductions of Monographs and Serials, Version 1. Digital Library Federation, December 2002. |u http://purl.oclc.org/DLF/benchrepro0212 |5 MiAaHDL | ||
| 583 | 1 | |a digitized |c 2013 |h HathiTrust Digital Library |l committed to preserve |2 pda |5 MiAaHDL | |
| 588 | 0 | |a Print version record. | |
| 506 | |a Access restricted to Ryerson students, faculty and staff. |5 CaOTR | ||
| 590 | |a Knovel |b ACADEMIC - Aerospace & Radar Technology | ||
| 650 | 0 | |a Strains and stresses. | |
| 650 | 0 | |a Aerodynamics |x Research. | |
| 650 | 6 | |a Contraintes (Mécanique) | |
| 650 | 6 | |a Aérodynamique |x Recherche. | |
| 650 | 7 | |a Aerodynamics |x Research. |2 fast |0 (OCoLC)fst00798205 | |
| 650 | 7 | |a Strains and stresses. |2 fast |0 (OCoLC)fst01134288 | |
| 700 | 1 | |a Duberg, John E. |q (John Edward), |d 1917- | |
| 700 | 1 | |a Diskin, Simon H. | |
| 710 | 2 | |a Langley Aeronautical Laboratory. | |
| 710 | 1 | |a United States. |b National Advisory Committee for Aeronautics. | |
| 776 | 0 | 8 | |i Print version: |a Kuhn, Paul. |t Stresses around rectangular cut-outs in skin-stringer panels under axial loads - II. |d Langley Field, VA : Langley Memorial Aeronautical Laboratory, 1943 |w (OCoLC)124075771 |
| 810 | 1 | |a United States. |b National Advisory Committee for Aeronautics. |t Wartime report ; |v L-368. | |
| 856 | 4 | 0 | |u https://appknovel.uam.elogim.com/kn/resources/kpSRCSSPA2/toc |z Texto completo |
| 994 | |a 92 |b IZTAP | ||