Nonlinear large-deflection boundary-value problems of rectangular plates

Relaxation and successive approximation methods are used to solve Von Karman's equations as applied to initially flat, rectangular plates with large deflections under either normal pressure or combined normal pressure and side thrust, and several specific cases are analyzed. The general method...

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Bibliographic Details
Main Author: Wang, Chi-Teh, (Author)
Format: eBook
Language: English
Published: Washington, D.C. : National Advisory Committee for Aeronautics, 1948.
Series: Technical note (United States. National Advisory Committee for Aeronautics) ; no. 1425.
Subjects:
Plates (Engineering)
Boundary value problems.
Relaxation methods (Mathematics)
elektronické knihy
electronic books
ISBN: 9781680156096
1680156098
Physical Description: 1 online resource (113 pages) : illustrations, tables

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Table of contents

LEADER 02674cam a2200421 i 4500
001 kn-ocn919093613
003 OCoLC
005 20240717213016.0
006 m o d
007 cr cn|||||||||
008 150824s1948 dcuad 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 OCLCO  |d OCLCQ  |d UPM  |d OCLCQ  |d OCLCO  |d OCLCL  |d SXB 
020 |a 9781680156096  |q (electronic bk.) 
020 |a 1680156098  |q (electronic bk.) 
035 |a (OCoLC)919093613 
100 1 |a Wang, Chi-Teh,  |e author. 
245 1 0 |a Nonlinear large-deflection boundary-value problems of rectangular plates /  |c by Chi-Teh Wang. 
264 1 |a Washington, D.C. :  |b National Advisory Committee for Aeronautics,  |c 1948. 
300 |a 1 online resource (113 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 1425 
500 |a Date of issue: March 1948. 
500 |a Report no. NACA TN No. 1425. 
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 Relaxation and successive approximation methods are used to solve Von Karman's equations as applied to initially flat, rectangular plates with large deflections under either normal pressure or combined normal pressure and side thrust, and several specific cases are analyzed. The general method developed may be applied to bending and combined bending and buckling problems with practically any boundary conditions to any required degree of accuracy or applied to solve the membrane theory of the plate which applies when the deflection is very large in comparison with the thickness of the plate. 
590 |a Knovel  |b Knovel (All titles) 
650 0 |a Plates (Engineering) 
650 0 |a Boundary value problems. 
650 0 |a Relaxation methods (Mathematics) 
655 7 |a elektronické knihy  |7 fd186907  |2 czenas 
655 9 |a electronic books  |2 eczenas 
710 1 |a United States.  |b National Advisory Committee for Aeronautics,  |e issuing body. 
776 0 8 |i Print version:  |a Wang, Chi-Teh.  |t Nonlinear large-deflection boundary-value problems of rectangular plates  |w (OCoLC)656395082 
830 0 |a Technical note (United States. National Advisory Committee for Aeronautics) ;  |v no. 1425. 
856 4 0 |u https://proxy.k.utb.cz/login?url=https://app.knovel.com/hotlink/toc/id:kpNLDBVPR6/nonlinear-large-deflection?kpromoter=marc  |y Full text 

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