The stability under longitudinal compression of flat symmetric corrugated-core sandwich plates with simply supported loaded edges and simply supported or clamped unloaded edges

A theory for the elastic behavior of orthotropic sandwich plates is used to determine the compressive buckling-load parameters of flat symmetrical corrugated core sandwich plates with simply supported loaded edges and simply supported or clamped unloaded edges.

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Bibliographic Details
Main Author: Seide, Paul, (Author)
Corporate Authors: Langley Aeronautical Laboratory., United States. National Advisory Committee for Aeronautics.
Format: eBook
Language: English
Published: Washington, D.C. : National Advisory Committee for Aeronautics, 1952.
Series: Technical note (United States. National Advisory Committee for Aeronautics) ; no. 2679.
Subjects:
Plates (Engineering)
Sandwich construction.
Loads (Mechanics)
Buckling (Mechanics)
Elasticity.
elektronické knihy
electronic books
ISBN: 9781680156249
1680156241
Physical Description: 1 online resource (30 pages) : illustrations

Cover

Table of contents

LEADER 02623cam a2200469 i 4500
001 kn-ocn919140207
003 OCoLC
005 20240717213016.0
006 m o d
007 cr cn|||||||||
008 150825s1952 dcua obt f000 0 eng d
040 |a KNOVL  |b eng  |e rda  |e pn  |c KNOVL  |d ZCU  |d UAB  |d DKU  |d OCLCQ  |d CEF  |d RRP  |d YOU  |d S2H  |d OCLCO  |d COP  |d OCLCQ  |d OCLCO  |d OCLCL  |d SXB 
020 |a 9781680156249  |q (electronic bk.) 
020 |a 1680156241  |q (electronic bk.) 
035 |a (OCoLC)919140207 
100 1 |a Seide, Paul,  |e author. 
245 1 4 |a The stability under longitudinal compression of flat symmetric corrugated-core sandwich plates with simply supported loaded edges and simply supported or clamped unloaded edges /  |c Paul Seide. 
264 1 |a Washington, D.C. :  |b National Advisory Committee for Aeronautics,  |c 1952. 
300 |a 1 online resource (30 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 2679 
500 |a "Langley Aeronautical Laboratory." 
500 |a Date of issue: April 1952. 
500 |a Report no. NACA-TN-2679. 
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 theory for the elastic behavior of orthotropic sandwich plates is used to determine the compressive buckling-load parameters of flat symmetrical corrugated core sandwich plates with simply supported loaded edges and simply supported or clamped unloaded edges. 
504 |a Includes bibliographical references (page 19) 
590 |a Knovel  |b Knovel (All titles) 
650 0 |a Plates (Engineering) 
650 0 |a Sandwich construction. 
650 0 |a Loads (Mechanics) 
650 0 |a Buckling (Mechanics) 
650 0 |a Elasticity. 
655 7 |a elektronické knihy  |7 fd186907  |2 czenas 
655 9 |a electronic books  |2 eczenas 
710 2 |a Langley Aeronautical Laboratory. 
710 1 |a United States.  |b National Advisory Committee for Aeronautics. 
776 0 8 |i Print version:  |a Seide, Paul.  |t Stability under longitudinal compression of flat symmetric corrugated-core sandwich plates with simply supported loaded edges and simply supported or clamped unloaded edges  |w (OCoLC)667231146 
830 0 |a Technical note (United States. National Advisory Committee for Aeronautics) ;  |v no. 2679. 
856 4 0 |u https://proxy.k.utb.cz/login?url=https://app.knovel.com/hotlink/toc/id:kpSLCFSCC2/stability-under-longitudinal?kpromoter=marc  |y Full text 

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