Tension fields in originally curved, thin sheets during shearing stresses

The analysis of the stresses in the sheet and stiffeners is predicated upon the direction of the wrinkles, particularly the tensile stresses (principal stresses). This analysis and the calculation of stresses after buckling form the subject of the present article. It includes: 1) metal cylinders wit...

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Bibliographic Details
Main Authors: Wagner, H., (Author), Ballerstedt, W., (Author)
Corporate Author: United States. National Advisory Commitee for Aeronautics.
Format: eBook
Language: English
Published: Washington, D.C. : National Advisory Commitee for Aeronautics, [1935]
Series: Technical memorandum (United States. National Advisory Committee for Aeronautics) ; no. 774.
Subjects:
Shells (Engineering)
Thin-walled structures.
Curvature.
Shear (Mechanics)
Strains and stresses.
elektronické knihy
electronic books
ISBN: 9781680156577
1680156578
Physical Description: 1 online resource (11 pages, 2 unnumbered pages) : illustrations

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Table of contents

LEADER 02772cam a2200481 i 4500
001 kn-ocn919168137
003 OCoLC
005 20240717213016.0
006 m o d
007 cr cn|||||||||
008 150825s1935 dcua obt f000 0 eng d
040 |a KNOVL  |b eng  |e rda  |e pn  |c KNOVL  |d OCLCE  |d ZCU  |d OCLCQ  |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 9781680156577  |q (electronic bk.) 
020 |a 1680156578  |q (electronic bk.) 
035 |a (OCoLC)919168137  |z (OCoLC)297432259  |z (OCoLC)608168843  |z (OCoLC)977309390  |z (OCoLC)987643080  |z (OCoLC)1047743383  |z (OCoLC)1229061459 
042 |a dlr 
100 1 |a Wagner, H.,  |e author. 
245 1 0 |a Tension fields in originally curved, thin sheets during shearing stresses /  |c H. Wagner and W. Ballerstedt. 
264 1 |a Washington, D.C. :  |b National Advisory Commitee for Aeronautics,  |c [1935] 
300 |a 1 online resource (11 pages, 2 unnumbered 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 Technical memorandums ;  |v number 774 
500 |a "August 1935." 
500 |a NACA TM No. 774. 
500 |a Translated from Luftfahrtforschung. Vol. 12, No. 2, pp. 70-74, May 16, 1935, by the National Advisory Commitee for Aeronautics. 
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 The analysis of the stresses in the sheet and stiffeners is predicated upon the direction of the wrinkles, particularly the tensile stresses (principal stresses). This analysis and the calculation of stresses after buckling form the subject of the present article. It includes: 1) metal cylinders with closely spaced longitudinal stiffeners; 2) metal cylinders with closely spaced transverse rings. 
590 |a Knovel  |b Knovel (All titles) 
650 0 |a Shells (Engineering) 
650 0 |a Thin-walled structures. 
650 0 |a Curvature. 
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 Ballerstedt, W.,  |e author. 
710 1 |a United States.  |b National Advisory Commitee for Aeronautics. 
776 0 8 |i Print version:  |a Wagner, H.  |t Tension fields in originally curved, thin sheets during shearing stresses  |w (OCoLC)696180837 
830 0 |a Technical memorandum (United States. National Advisory Committee for Aeronautics) ;  |v no. 774. 
856 4 0 |u https://proxy.k.utb.cz/login?url=https://app.knovel.com/hotlink/toc/id:kpTFOCTSS1/tension-fields-in?kpromoter=marc  |y Full text 

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