Rectangular shell plating under uniformly distributed hydrostatic pressure

A check of the calculation methods used by Foppl and Henky for investigating the reliability of shell plating under hydrostatic pressure has proved that the formulas yield practical results within the elastic range of the material. Foppl's approximate calculation leaves one on the safe side. It...

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Bibliographic Details
Main Authors: Neubert, M., (Author), Sommer, A., (Author)
Corporate Author: United States. National Advisory Commitee for Aeronautics.
Format: eBook
Language: English
Published: Washington, D.C. : National Advisory Commitee for Aeronautics, [1940]
Series: Technical memorandum (United States. National Advisory Committee for Aeronautics) ; no. 965.
Subjects:
Shells (Engineering)
Plates (Engineering)
Hydrostatic pressure.
Strains and stresses.
Mathematics.
elektronické knihy
electronic books
ISBN: 9781680156553
1680156551
Physical Description: 1 online resource (7 pages, 3 unnumbered pages) : illustrations

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LEADER 02884cam a2200481 i 4500
001 kn-ocn919167769
003 OCoLC
005 20240717213016.0
006 m o d
007 cr cn|||||||||
008 150825s1940 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 YOU  |d OCLCE  |d S2H  |d OCLCO  |d OCLCQ  |d UPM  |d OCLCQ  |d COP  |d OCLCO  |d SXB 
020 |a 9781680156553  |q (electronic bk.) 
020 |a 1680156551  |q (electronic bk.) 
035 |a (OCoLC)919167769  |z (OCoLC)1111582256  |z (OCoLC)1116072624  |z (OCoLC)1229060563 
042 |a dlr 
100 1 |a Neubert, M.,  |e author. 
245 1 0 |a Rectangular shell plating under uniformly distributed hydrostatic pressure /  |c by M. Neubert and A. Sommer. 
264 1 |a Washington, D.C. :  |b National Advisory Commitee for Aeronautics,  |c [1940] 
300 |a 1 online resource (7 pages, 3 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 National Advisory Committee for Aeronautics technical memorandums ; ‡v 965 
500 |a "December 1940." 
500 |a NACA TM No. 965. 
500 |a Translated from Luftfahrtforschung. Vol. 17, No. 7, pp. 207-210, July 20, 1940, by the National Advisory Commitee for Aeronautics. 
504 |a Includes bibliographical references (page 7) 
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 check of the calculation methods used by Foppl and Henky for investigating the reliability of shell plating under hydrostatic pressure has proved that the formulas yield practical results within the elastic range of the material. Foppl's approximate calculation leaves one on the safe side. It further was found on the basis of the marked ductility of the shell plating under tensile stress that the strength is from 50 to 100 percent higher in the elastic range than expected by either method. 
590 |a Knovel  |b Knovel (All titles) 
650 0 |a Shells (Engineering) 
650 0 |a Plates (Engineering) 
650 0 |a Hydrostatic pressure. 
650 0 |a Strains and stresses. 
650 0 |a Mathematics. 
655 7 |a elektronické knihy  |7 fd186907  |2 czenas 
655 9 |a electronic books  |2 eczenas 
700 1 |a Sommer, A.,  |e author. 
710 1 |a United States.  |b National Advisory Commitee for Aeronautics. 
776 0 8 |i Print version:  |a Neubert, M.  |t Rectangular shell plating under uniformly distributed hydrostatic pressure  |w (OCoLC)697281935 
830 0 |a Technical memorandum (United States. National Advisory Committee for Aeronautics) ;  |v no. 965. 
856 4 0 |u https://proxy.k.utb.cz/login?url=https://app.knovel.com/hotlink/toc/id:kpRSPUDHP1/rectangular-shell-plating?kpromoter=marc  |y Full text 

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