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...
Saved in:
| Main Author | |
|---|---|
| Corporate Authors | , |
| Other Authors | , |
| Format | Electronic eBook |
| Language | English |
| Published |
Langley Field, VA :
Langley Memorial Aeronautical Laboratory,
1943.
|
| Series | NACA WR ;
L-368 |
| Subjects | |
| Online Access | Full text |
| ISBN | 9781680156485 1680156489 |
| Physical Description | 1 online resource (46 pages, [32] leaves) : illustrations |
Cover
| LEADER | 00000cam a2200000 a 4500 | ||
|---|---|---|---|
| 001 | kn-ocn857368754 | ||
| 003 | OCoLC | ||
| 005 | 20240717213016.0 | ||
| 006 | m o d | ||
| 007 | cr cn||||||||| | ||
| 008 | 130901e194310 vauado obt f000 0 eng d | ||
| 040 | |a OCLCE |b eng |e pn |c OCLCE |d OCLCA |d OCLCQ |d OCLCF |d KNOVL |d ZCU |d OCLCQ |d UAB |d OCLCQ |d CEF |d RRP |d YOU |d S2H |d OCLCO |d OCLCQ |d OCLCO |d OCLCQ |d OCLCO |d OCLCL |d SXB | ||
| 020 | |a 9781680156485 |q (electronic bk.) | ||
| 020 | |a 1680156489 |q (electronic bk.) | ||
| 035 | |a (OCoLC)857368754 |z (OCoLC)951660439 |z (OCoLC)977856136 |z (OCoLC)987733981 |z (OCoLC)1047754267 |z (OCoLC)1229061830 | ||
| 042 | |a dlr | ||
| 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). | ||
| 506 | |a Plný text je dostupný pouze z IP adres počítačů Univerzity Tomáše Bati ve Zlíně nebo vzdáleným přístupem pro zaměstnance a studenty | ||
| 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. | ||
| 590 | |a Knovel |b Knovel (All titles) | ||
| 650 | 0 | |a Strains and stresses. | |
| 650 | 0 | |a Aerodynamics |x Research. | |
| 655 | 7 | |a elektronické knihy |7 fd186907 |2 czenas | |
| 655 | 9 | |a electronic books |2 eczenas | |
| 700 | 1 | |a Duberg, John E. |q (John Edward), |d 1917- |1 https://id.oclc.org/worldcat/entity/E39PCjDygMkbpcWM9WqyPkYQMP | |
| 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://proxy.k.utb.cz/login?url=https://app.knovel.com/hotlink/toc/id:kpSRCSSPA2/stresses-around-rectangular?kpromoter=marc |y Full text |