Square plate with clamped edges under normal pressure producing large deflections

A theoretical analysis is given for the stresses and deflections of a square plate with clamped edges under normal pressure producing large deflections. Values of the bending stress and membrane stress at the center of the plate and at the midpoint of the edge are given for center deflections up to...

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Bibliographic Details
Main Author: Levy, Samuel, (Author)
Format: eBook
Language: English
Published: Washington, [D.C.] : National Advisory Committee for Aeronautics, 1942.
Series: Technical note (United States. National Advisory Committee for Aeronautics) ; 847.
Subjects:
Plates (Engineering)
Loads (Mechanics)
Aeronautics > Research.
Airplanes > Design and construction.
Strains and stresses > Analysis.
elektronické knihy
electronic books
ISBN: 9781680156430
1680156438
Physical Description: 1 online resource (25 pages, 5 unnumbered pages) : illustrations.

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Table of contents

LEADER 02859cam a2200457 i 4500
001 kn-ocn919151114
003 OCoLC
005 20240717213016.0
006 m o d
007 cr cn|||||||||
008 150825s1942 dcua ob f000 0 eng c
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 TRAAL  |d S2H  |d OCLCO  |d GPO  |d OCLCO  |d OCL  |d OCLCO  |d SXB 
020 |a 9781680156430  |q electronic bk. 
020 |a 1680156438  |q electronic bk. 
035 |a (OCoLC)919151114  |z (OCoLC)1164733650 
042 |a pcc 
100 1 |a Levy, Samuel,  |e author. 
245 1 0 |a Square plate with clamped edges under normal pressure producing large deflections /  |c by Samuel Levy. 
264 1 |a Washington, [D.C.] :  |b National Advisory Committee for Aeronautics,  |c 1942. 
300 |a 1 online resource (25 pages, 5 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 notes / National Advisory Committee for Aeronautics ;  |v no. 847 
500 |a "May 1942." 
500 |a No Federal Depository Library Program (FDLP) item number. 
504 |a Includes bibliographical references (pages 17-18). 
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 A theoretical analysis is given for the stresses and deflections of a square plate with clamped edges under normal pressure producing large deflections. Values of the bending stress and membrane stress at the center of the plate and at the midpoint of the edge are given for center deflections up to 1.9 times the plate thickness. The shape of the deflected surface is given for low pressures and for the highest pressure considered. Convergence of solution is considered and it is estimated that the possible error is less than 2 percent. --  |c Provided by publisher. 
590 |a Knovel  |b Knovel (All titles) 
650 0 |a Plates (Engineering) 
650 0 |a Loads (Mechanics) 
650 0 |a Aeronautics  |x Research. 
650 0 |a Airplanes  |x Design and construction. 
650 0 |a Strains and stresses  |x Analysis. 
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 Levy, Samuel.  |t Square plate with clamped edges under normal pressure producing large deflections.  |d Washington D.C. : National Advisory Committee for Aeronautics, 1942  |w (OCoLC)646863696 
830 0 |a Technical note (United States. National Advisory Committee for Aeronautics) ;  |v 847. 
856 4 0 |u https://proxy.k.utb.cz/login?url=https://app.knovel.com/hotlink/toc/id:kpSPCENPP1/square-plate-with?kpromoter=marc  |y Full text 

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