Critical combinations of shear and longitudinal direct stress for long plates with transverse curvature

A theoretical solution is presented for the buckling stresses of long plates with transverse curvature loaded in shear and longitudinal direct stress. The theoretical critical-stress combinations for plates having either simply supported or clamped edges are given in figures and tables and a compari...

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Bibliographic Details
Main Authors: Batdorf, S. B., (Author), Schildcrout, Murry, (Author), Stein, Manuel, (Author)
Corporate Author: Langley Aeronautical Laboratory.
Format: eBook
Language: English
Published: Washington, D.C. : National Advisory Committee for Aeronautics, 1947.
Series: Technical note (United States. National Advisory Committee for Aeronautics) ; no. 1347.
Subjects:
Plates (Engineering)
Strains and stresses.
Buckling (Mechanics)
Loads (Mechanics)
Shear (Mechanics)
elektronické knihy
electronic books
ISBN: 9781680156065
1680156063
Physical Description: 1 online resource (27 pages, 9 unnumbered pages) : illustrations, tables

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LEADER 02853cam a2200493 i 4500
001 kn-ocn919093316
003 OCoLC
005 20240717213016.0
006 m o d
007 cr cn|||||||||
008 150824s1947 dcua obt f000 0 eng d
040 |a KNOVL  |b eng  |e rda  |e pn  |c KNOVL  |d ZCU  |d OCLCQ  |d UAB  |d DKU  |d OCLCQ  |d CEF  |d RRP  |d WYU  |d YOU  |d S2H  |d OCLCO  |d COP  |d OCLCO  |d COP  |d OCLCO  |d OCLCQ  |d UPM  |d OCLCQ  |d OCLCO  |d OCLCL  |d SXB 
020 |a 9781680156065  |q (electronic bk.) 
020 |a 1680156063  |q (electronic bk.) 
035 |a (OCoLC)919093316 
100 1 |a Batdorf, S. B.,  |e author. 
245 1 0 |a Critical combinations of shear and longitudinal direct stress for long plates with transverse curvature /  |c by S.B. Batdort, Murry Schildcrout, and Manuel Stein. 
264 1 |a Washington, D.C. :  |b National Advisory Committee for Aeronautics,  |c 1947. 
300 |a 1 online resource (27 pages, 9 unnumbered pages) :  |b illustrations, tables 
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 technical note ;  |v number 1347 
500 |a "Langley Memorial Aeronautical Laboratory." 
500 |a Date of issue: June 1947. 
500 |a Report no. NACA TN No. 1347. 
504 |a Includes bibliographical references (pages 23-24) 
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 theoretical solution is presented for the buckling stresses of long plates with transverse curvature loaded in shear and longitudinal direct stress. The theoretical critical-stress combinations for plates having either simply supported or clamped edges are given in figures and tables and a comparison is made with a previous theoretical solution for simply supported plates. 
590 |a Knovel  |b Knovel (All titles) 
650 0 |a Plates (Engineering) 
650 0 |a Strains and stresses. 
650 0 |a Buckling (Mechanics) 
650 0 |a Loads (Mechanics) 
650 0 |a Shear (Mechanics) 
655 7 |a elektronické knihy  |7 fd186907  |2 czenas 
655 9 |a electronic books  |2 eczenas 
700 1 |a Schildcrout, Murry,  |e author. 
700 1 |a Stein, Manuel,  |e author. 
710 1 |a United States.  |b National Advisory Committee for Aeronautics,  |e issuing body. 
710 2 |a Langley Aeronautical Laboratory. 
776 0 8 |i Print version:  |a Batdorf, S.B.  |t Critical combinations of shear and longitudinal direct stress for long plates with transverse curvature  |w (OCoLC)652540878 
830 0 |a Technical note (United States. National Advisory Committee for Aeronautics) ;  |v no. 1347. 
856 4 0 |u https://proxy.k.utb.cz/login?url=https://app.knovel.com/hotlink/toc/id:kpCCSLDSL1/critical-combinations-of?kpromoter=marc  |y Full text 

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