Approximate stress analysis of multistringer beams with shear deformation of the flanges
The problem of the skin-stringer combinations used as axially loaded panels or as covers for box beams is considered from the point of view of the practical stress analyst. By a simple substitution the problem is reduced to the problem of the single-stringer structure, which has been treated in NACA...
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Main Author: | |
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Corporate Authors: | , |
Format: | eBook |
Language: | English |
Published: |
Washington, D.C. :
U.S. Government Printing Office,
1938.
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Series: | Report (United States. National Advisory Committee for Aeronautics) ;
no. 636. |
Subjects: | |
ISBN: | 9781680156409 1680156403 |
Physical Description: | 1 online resource (ii, 21 pages) : illustrations |
LEADER | 02598cam a2200409 i 4500 | ||
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001 | kn-ocn919150706 | ||
003 | OCoLC | ||
005 | 20240717213016.0 | ||
006 | m o d | ||
007 | cr cn||||||||| | ||
008 | 150825s1938 dcua ob f000 0 eng d | ||
040 | |a KNOVL |b eng |e rda |e pn |c KNOVL |d OCLCF |d ZCU |d UAB |d DKU |d OCLCQ |d CEF |d RRP |d YOU |d S2H |d OCLCO |d OCLCQ |d UPM |d OCLCQ |d OCLCO |d SXB | ||
020 | |a 9781680156409 |q (electronic bk.) | ||
020 | |a 1680156403 |q (electronic bk.) | ||
035 | |a (OCoLC)919150706 | ||
100 | 1 | |a Kuhn, Paul. | |
245 | 1 | 0 | |a Approximate stress analysis of multistringer beams with shear deformation of the flanges / |c by Paul Kuhn. |
264 | 1 | |a Washington, D.C. : |b U.S. Government Printing Office, |c 1938. | |
300 | |a 1 online resource (ii, 21 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 Report / National Advisory Committee for Aeronautics ; |v number 636 | |
504 | |a Includes bibliographical references (page 21). | ||
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 The problem of the skin-stringer combinations used as axially loaded panels or as covers for box beams is considered from the point of view of the practical stress analyst. By a simple substitution the problem is reduced to the problem of the single-stringer structure, which has been treated in NACA Report no. 608. The method of making this substitution is essentially empirical; in order to justify it, comparisons are shown between calculations and strain-gage tests of three beams tested by the author and of one compression panel and three beams tested and reported elsewhere. -- |c Provided by publisher. | ||
590 | |a Knovel |b Knovel (All titles) | ||
650 | 0 | |a Shear (Mechanics) | |
650 | 0 | |a Deformations (Mechanics) | |
650 | 0 | |a Strains and stresses. | |
655 | 7 | |a elektronické knihy |7 fd186907 |2 czenas | |
655 | 9 | |a electronic books |2 eczenas | |
710 | 1 | |a United States. |b National Advisory Committee for Aeronautics. | |
710 | 2 | |a Langley Aeronautical Laboratory. | |
776 | 0 | 8 | |i Print version: |a Kuhn, Paul. |t Approximate stress analysis of multistringer beams with shear deformation of the flanges |w (OCoLC)918949241 |
830 | 0 | |a Report (United States. National Advisory Committee for Aeronautics) ; |v no. 636. | |
856 | 4 | 0 | |u https://proxy.k.utb.cz/login?url=https://app.knovel.com/hotlink/toc/id:kpASAMBSD2/approximate-stress-analysis?kpromoter=marc |y Full text |