Bending of rectangular plates with large deflections

The solution of Von Karman's fundamental equations for large deflections of plates is presented for the case of a simply supported rectangular plate under combined edge compression and lateral loading. Numerical solutions are given for square plates and for rectangular plates with a width-span...

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Bibliographic Details
Main Author: Levy, Samuel.
Corporate Author: United States. National Advisory Committee for Aeronautics.
Format: eBook
Language: English
Published: Washington, D.C. : G.P.O., 1942.
Series: Report (United States. National Advisory Committee for Aeronautics) ; no. 737.
Subjects:
Aeronautics > Research.
Airplanes > Design and construction.
elektronické knihy
electronic books
ISBN: 9781680156416
1680156411
Physical Description: 1 online resource (19 pages)

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Table of contents

LEADER 02215cam a2200397 i 4500
001 kn-ocn914548959
003 OCoLC
005 20240717213016.0
006 m o d
007 cr cn|||||||||
008 150727s1942 dcu ob 000 0 eng d
040 |a SINTU  |b eng  |e pn  |c SINTU  |d KNOVL  |d ZCU  |d OCLCQ  |d UAB  |d DKU  |d OCLCQ  |d CEF  |d RRP  |d YOU  |d S2H  |d OCLCO  |d OCLCQ  |d OCLCO  |d OCLCQ  |d OCLCO  |d OCLCL  |d SXB 
020 |a 9781680156416  |q (electronic bk.) 
020 |a 1680156411  |q (electronic bk.) 
035 |a (OCoLC)914548959  |z (OCoLC)951666776 
100 1 |a Levy, Samuel. 
245 1 0 |a Bending of rectangular plates with large deflections /  |c by Samuel Levy. 
260 |a Washington, D.C. :  |b G.P.O.,  |c 1942. 
300 |a 1 online resource (19 pages) 
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 no. 737 
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 |a The solution of Von Karman's fundamental equations for large deflections of plates is presented for the case of a simply supported rectangular plate under combined edge compression and lateral loading. Numerical solutions are given for square plates and for rectangular plates with a width-span ratio of 3:1. --  |c Provided by publisher. 
590 |a Knovel  |b Knovel (All titles) 
650 0 |a Aeronautics  |x Research. 
650 0 |a Airplanes  |x Design and construction. 
655 7 |a elektronické knihy  |7 fd186907  |2 czenas 
655 9 |a electronic books  |2 eczenas 
700 1 |a Levy, Samuel. 
710 1 |a United States.  |b National Advisory Committee for Aeronautics. 
776 0 8 |i Print version:  |a Levy, Samuel.  |t Bending of rectangular plates with large deflections.  |d Washington, D.C. : G.P.O., 1942  |w (OCoLC)46827401 
830 0 |a Report (United States. National Advisory Committee for Aeronautics) ;  |v no. 737. 
856 4 0 |u https://proxy.k.utb.cz/login?url=https://app.knovel.com/hotlink/toc/id:kpBRPLDN01/bending-of-rectangular?kpromoter=marc  |y Full text 

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