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

Results are presented of tests of two sets of 20 curved-sheet specimens to determine the effect of normal pressure on the critical compressive and shear stress of curved sheet. It was found that normal pressure raised the critical compressive and shear stress of curved sheet except when outward bulg...

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Bibliographic Details
Main Author: Rafel, Norman.
Corporate Authors: United States. National Advisory Committee for Aeronautics., Langley Aeronautical Laboratory.
Other Authors: Sandlin, Charles W.
Format: eBook
Language: English
Published: Washington, D.C. : National Advisory Committee for Aeronautics, [1945]
Series: Wartime Reports (United States. National Advisory Committee for Aeronautics) ; no. L57.
Subjects:
Box beams.
Aluminum alloys.
Plates (Engineering) > Curvature.
Loads (Mechanics)
Shear (Mechanics)
Buckling (Mechanics)
Strains and stresses.
Charts, diagrams, etc.
elektronické knihy
electronic books
ISBN: 9781680156355
1680156357
Physical Description: 1 online resource (7, [8] pages) : illustrations

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Table of contents

LEADER 03028cam a2200529 i 4500
001 kn-ocn914330037
003 OCoLC
005 20240717213016.0
006 m o d
007 cr cn|||||||||
008 150724s1945 dcua obt f000 0 eng d
040 |a SINTU  |b eng  |e pn  |c SINTU  |d SINTU  |d OCLCO  |d KNOVL  |d ZCU  |d OCLCQ  |d UAB  |d DKU  |d OCLCF  |d OCLCQ  |d CEF  |d RRP  |d YOU  |d S2H  |d OCLCO  |d OCLCQ  |d OCLCO  |d OCLCQ  |d OCLCO  |d SXB 
020 |a 9781680156355  |q (electronic bk.) 
020 |a 1680156357  |q (electronic bk.) 
035 |a (OCoLC)914330037  |z (OCoLC)951668476 
100 1 |a Rafel, Norman. 
245 1 0 |a Effect of normal pressure on the critical compressive and shear stress of curved sheet /  |c Norman Rafel and Charles W. Sandlin, Jr. 
246 3 |a NACA Wartime Reports. Series L. 
260 |a Washington, D.C. :  |b National Advisory Committee for Aeronautics,  |c [1945] 
300 |a 1 online resource (7, [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. L57 
500 |a NACA Wartime Report L-57. 
500 |a Originally issued as NACA as Advance Restricted Report L5B10 (March 1945). 
500 |a Prepared at the Langley Memorial Aeronautical Laboratory, Langley Field, Virginia. 
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 Results are presented of tests of two sets of 20 curved-sheet specimens to determine the effect of normal pressure on the critical compressive and shear stress of curved sheet. It was found that normal pressure raised the critical compressive and shear stress of curved sheet except when outward bulging occurred in compression, in which case the critical stress was lowered by normal pressure. 
590 |a Knovel  |b Knovel (All titles) 
650 0 |a Box beams. 
650 0 |a Aluminum alloys. 
650 0 |a Plates (Engineering)  |x Curvature. 
650 0 |a Loads (Mechanics) 
650 0 |a Shear (Mechanics) 
650 0 |a Buckling (Mechanics) 
650 0 |a Strains and stresses. 
650 0 |a Charts, diagrams, etc. 
655 7 |a elektronické knihy  |7 fd186907  |2 czenas 
655 9 |a electronic books  |2 eczenas 
700 1 |a Sandlin, Charles W. 
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 and shear stress of curved sheet.  |d Washington, D.C. : National Advisory Committee for Aeronautics, [1945]  |w (OCoLC)705351009 
830 0 |a Wartime Reports (United States. National Advisory Committee for Aeronautics) ;  |v no. L57. 
856 4 0 |u https://proxy.k.utb.cz/login?url=https://app.knovel.com/hotlink/toc/id:kpENPCCSS3/effect-of-normal?kpromoter=marc  |y Full text 

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