Critical combinations of shear and direct axial stress for curved rectangular panels

A solution is presented for the problem of the buckling of curved rectangular panels subjected to combinded shear and direct axial stress. Charts giving theoretical critical combinations of shear and direct axial stress are presented for panels having five different length-width ratios.

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Bibliographic Details
Main Author: Schildcrout, Murry.
Corporate Author: United States. National Advisory Committee for Aeronautics.
Other Authors: Stein, Manuel.
Format: eBook
Language: English
Published: Washington, D.C. : National Advisory Committee for Aeronautics, 1949.
Series: Technical note (United States. National Advisory Committee for Aeronautics) ; no. 1928.
Subjects:
Plates (Engineering)
Curvature.
Buckling (Mechanics)
Shear (Mechanics)
Strains and stresses.
elektronické knihy
electronic books
ISBN: 9781680156164
1680156160
Physical Description: 1 online resource (29 pages) : illustrations

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Table of contents

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001 kn-ocn914328363
003 OCoLC
005 20240717213016.0
006 m o d
007 cr cn|||||||||
008 150724s1949 ohua obt f000 0 eng d
040 |a SINTU  |b eng  |e pn  |c SINTU  |d SINTU  |d KNOVL  |d ZCU  |d OCLCQ  |d UAB  |d DKU  |d OCLCQ  |d CEF  |d RRP  |d WYU  |d YOU  |d S2H  |d OCLCO  |d TRAAL  |d OCLCQ  |d OCLCO  |d OCLCQ  |d OCLCO  |d OCLCL  |d SXB 
020 |a 9781680156164  |q (electronic bk.) 
020 |a 1680156160  |q (electronic bk.) 
035 |a (OCoLC)914328363  |z (OCoLC)951667867 
100 1 |a Schildcrout, Murry. 
245 1 0 |a Critical combinations of shear and direct axial stress for curved rectangular panels /  |c Murry Schildcrout and Manuel Stein. 
260 |a Washington, D.C. :  |b National Advisory Committee for Aeronautics,  |c 1949. 
300 |a 1 online resource (29 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 National Advisory Committee for Aeronautics ;  |v no. 1928 
500 |a "August 1949." 
500 |a NACA TN No. 1928. 
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 A solution is presented for the problem of the buckling of curved rectangular panels subjected to combinded shear and direct axial stress. Charts giving theoretical critical combinations of shear and direct axial stress are presented for panels having five different length-width ratios. 
520 3 |a Because the actual critical compressive stress of rectangular panels having substantial curvature is known to be much lower than the theoretical value, a semi-empirical method of analysis of curved panels subjected to combined shear and direct axial stress is presented for use in design. 
590 |a Knovel  |b Knovel (All titles) 
650 0 |a Plates (Engineering) 
650 0 |a Curvature. 
650 0 |a Buckling (Mechanics) 
650 0 |a Shear (Mechanics) 
650 0 |a Strains and stresses. 
655 7 |a elektronické knihy  |7 fd186907  |2 czenas 
655 9 |a electronic books  |2 eczenas 
700 1 |a Stein, Manuel. 
710 1 |a United States.  |b National Advisory Committee for Aeronautics. 
776 0 8 |i Print version:  |a Schildcrout, Murry.  |t Critical combinations of shear and direct axial stress for curved rectangular panels.  |d Washington, D.C. : National Advisory Committee for Aeronautics, 1949  |w (OCoLC)660169956 
830 0 |a Technical note (United States. National Advisory Committee for Aeronautics) ;  |v no. 1928. 
856 4 0 |u https://proxy.k.utb.cz/login?url=https://app.knovel.com/hotlink/toc/id:kpCCSDASC1/critical-combinations-of?kpromoter=marc  |y Full text 

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