Effect of normal pressure on the critical compressive stress of curved sheet

Results are presented of tests of two specimens tested to study the effect of normal pressure on the critical compressive stress for thin curved sheets. These specimens are designated by their respective rib spacings of 10 inches and 30 inches. The relationship between compressive stress and normal...

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Bibliographic Details
Main Author: Rafel, Norman.
Corporate Authors: United States. National Advisory Committee for Aeronautics., Langley Aeronautical Laboratory.
Format: eBook
Language: English
Published: Washington, D.C. : National Advisory Committee for Aeronautics, [1942]
Series: Wartime Reports (United States. National Advisory Committee for Aeronautics) ; no. L258.
Subjects:
Atmospheric pressure.
Buckling (Mechanics)
Strains and stresses.
Loads (Mechanics)
Charts, diagrams, etc.
elektronické knihy
electronic books
ISBN: 9781680156348
1680156349
Physical Description: 1 online resource (2, [8] pages) : illustrations

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Table of contents

LEADER 02832cam a2200469 i 4500
001 kn-ocn914330185
003 OCoLC
005 20240717213016.0
006 m o d
007 cr cn|||||||||
008 150724s1942 dcua ot f000 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 SXB 
020 |a 9781680156348  |q (electronic bk.) 
020 |a 1680156349  |q (electronic bk.) 
035 |a (OCoLC)914330185  |z (OCoLC)951667782 
100 1 |a Rafel, Norman. 
245 1 0 |a Effect of normal pressure on the critical compressive stress of curved sheet /  |c Norman Rafel. 
246 3 |a NACA Wartime Reports. Series L. 
260 |a Washington, D.C. :  |b National Advisory Committee for Aeronautics,  |c [1942] 
300 |a 1 online resource (2, [8] 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 Wartime Report / National Advisory Committee for Aeronautics ;  |v no. L258 
500 |a NACA Wartime Report L-258. 
500 |a Originally issued as NACA as a Restricted Bulletin (November 1942). 
500 |a Prepared at the Langley Memorial Aeronautical Laboratory, Langley Field, Virginia. 
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 Results are presented of tests of two specimens tested to study the effect of normal pressure on the critical compressive stress for thin curved sheets. These specimens are designated by their respective rib spacings of 10 inches and 30 inches. The relationship between compressive stress and normal pressure at which buckles disappeared is independent of whether the buckles were made to disappear by increase of normal pressure or decrease of compressive stress. 
590 |a Knovel  |b Knovel (All titles) 
650 0 |a Atmospheric pressure. 
650 0 |a Buckling (Mechanics) 
650 0 |a Strains and stresses. 
650 0 |a Loads (Mechanics) 
650 0 |a Charts, diagrams, etc. 
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. 
710 2 |a Langley Aeronautical Laboratory. 
776 0 8 |i Print version:  |a Rafel, Norman.  |t Effect of normal pressure on the critical compressive stress of curved sheet.  |d Washington, D.C. : National Advisory Committee for Aeronautics, [1942]  |w (OCoLC)707099582 
830 0 |a Wartime Reports (United States. National Advisory Committee for Aeronautics) ;  |v no. L258. 
856 4 0 |u https://proxy.k.utb.cz/login?url=https://app.knovel.com/hotlink/toc/id:kpENPCCSC1/effect-of-normal?kpromoter=marc  |y Full text 

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