Critical stress for an infinitely long flat plate with elastically restrained edges under combined shear and direct stress

A simple interaction curve is presented for evaluating the conditions of combined shear and direct stress under which an infinitely long, flat plate with equal elastic restraints against rotation along the edges will become unstable. The theoretical work that led to the interaction curve is presente...

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Bibliographic Details
Main Author: Stowell, Elbridge Z.
Corporate Authors: United States. National Advisory Committee for Aeronautics., Langley Aeronautical Laboratory.
Other Authors: Schwartz, Edward B.
Format: eBook
Language: English
Published: Washington, D.C. : National Advisory Committee for Aeronautics, [1943]
Series: Wartime Reports (United States. National Advisory Committee for Aeronautics) ; no. L340.
Subjects:
ISBN: 9781680156478
1680156470
Physical Description: 1 online resource (16, [3] pages) : illustrations

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Table of contents

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003 OCoLC
005 20240717213016.0
006 m o d
007 cr cn|||||||||
008 150727s1943 dcua obt 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 WYU  |d YOU  |d S2H  |d OCLCO  |d OCLCQ  |d OCLCO  |d OCLCQ  |d OCLCO  |d OCLCL  |d SXB  |d OCLCQ 
020 |a 9781680156478  |q (electronic bk.) 
020 |a 1680156470  |q (electronic bk.) 
035 |a (OCoLC)914552880  |z (OCoLC)951667803 
100 1 |a Stowell, Elbridge Z. 
245 1 0 |a Critical stress for an infinitely long flat plate with elastically restrained edges under combined shear and direct stress /  |c Elbridge Z. Stowell and Edward B. Schwartz. 
246 3 |a NACA Wartime Reports. Series L. 
260 |a Washington, D.C. :  |b National Advisory Committee for Aeronautics,  |c [1943] 
300 |a 1 online resource (16, [3] 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. L340 
500 |a NACA Wartime Report L-340. 
500 |a Originally issued as NACA as Advance Restricted Report L3K13 (November 1943). 
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 A simple interaction curve is presented for evaluating the conditions of combined shear and direct stress under which an infinitely long, flat plate with equal elastic restraints against rotation along the edges will become unstable. The theoretical work that led to the interaction curve is presented in the form of appendixes. 
590 |a Knovel  |b Knovel (All titles) 
650 0 |a Plates (Engineering) 
650 0 |a Shear (Mechanics) 
650 0 |a Buckling (Mechanics) 
650 0 |a Loads (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 Schwartz, Edward B. 
710 1 |a United States.  |b National Advisory Committee for Aeronautics. 
710 2 |a Langley Aeronautical Laboratory. 
776 0 8 |i Print version:  |a Stowell, Elbridge Z.  |t Critical stress for an infinitely long flat plate with elastically restrained edges under combined shear and direct stress.  |d Washington, D.C. : National Advisory Committee for Aeronautics, [1943]  |w (OCoLC)707629297 
830 0 |a Wartime Reports (United States. National Advisory Committee for Aeronautics) ;  |v no. L340. 
856 4 0 |u https://proxy.k.utb.cz/login?url=https://app.knovel.com/hotlink/toc/id:kpCSILFPE1/critical-stress-for?kpromoter=marc  |y Full text