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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Bibliographic Details
Main Author: Kuhn, Paul.
Corporate Authors: United States. National Advisory Committee for Aeronautics., Langley Aeronautical Laboratory.
Format: eBook
Language: English
Published: Washington, D.C. : U.S. Government Printing Office, 1938.
Series: Report (United States. National Advisory Committee for Aeronautics) ; no. 636.
Subjects:
ISBN: 9781680156409
1680156403
Physical Description: 1 online resource (ii, 21 pages) : illustrations

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Table of contents

LEADER 02598cam a2200409 i 4500
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