Critical combinations of longitudinal and transverse direct stress for an infinitely long flat plate with edges elastically restrained against rotation

A theoretical investigation was made of the buckling of an infinitely long flat plate with edges elastically restrained against rotation under combinations of longitudinal and transverse direct stress. Interaction curves are presented that give the critical combinations of stress for several differe...

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Bibliographic Details
Main Author Batdorf, S. B.
Corporate Authors Langley Aeronautical Laboratory, United States. National Advisory Committee for Aeronautics
Other Authors Stein, Manuel, Libove, Charles
Format Electronic eBook
LanguageEnglish
Published Langley Field, VA : Langley Memorial Aeronautical Laboratory, 1946.
SeriesNACA collection.
Subjects
Online AccessFull text
ISBN9781680156522
1680156527
Physical Description1 online resource (14, [6] pages)

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006 m o d
007 cr cn|||||||||
008 130901s1946 vauad obt f000 0 eng d
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020 |a 9781680156522  |q (electronic bk.) 
020 |a 1680156527  |q (electronic bk.) 
035 |a (OCoLC)857368708  |z (OCoLC)914554333  |z (OCoLC)951667684  |z (OCoLC)977336518  |z (OCoLC)987147222  |z (OCoLC)1047748312  |z (OCoLC)1229063615 
042 |a dlr 
100 1 |a Batdorf, S. B. 
245 1 0 |a Critical combinations of longitudinal and transverse direct stress for an infinitely long flat plate with edges elastically restrained against rotation /  |c S.B. Batdorf, Manuel Stein, and Charles Libove. 
246 3 |a NACA wartime reports 
260 |a Langley Field, VA :  |b Langley Memorial Aeronautical Laboratory,  |c 1946. 
300 |a 1 online resource (14, [6] pages) 
336 |a text  |b txt  |2 rdacontent 
337 |a computer  |b c  |2 rdamedia 
338 |a online resource  |b cr  |2 rdacarrier 
500 |a "Report no. L-49." 
500 |a "Originally issued March 1946 as Advance Restricted Report L6A05a." 
500 |a "NACA WARTIME REPORTS are reprints of papers originally issued to provide rapid distribution of advance research results to an authorized group requiring them for the war effort. They were previously held under a security status but are now unclassified. Some of these reports were not technically edited. All have been reproduced without change in order to expedite general distribution." 
504 |a Includes bibliographical references (page 13). 
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 investigation was made of the buckling of an infinitely long flat plate with edges elastically restrained against rotation under combinations of longitudinal and transverse direct stress. Interaction curves are presented that give the critical combinations of stress for several different degrees of elastic edge restraint, including simple support and complete fixity. It was found that an appreciable fraction of the critical longitudinal stress may be applied to the plate without any reduction in the transverse compressive stress required for buckling. 
590 |a Knovel  |b Knovel (All titles) 
650 0 |a Airplanes  |x Design and construction. 
650 0 |a Aerodynamics  |x Research. 
655 7 |a elektronické knihy  |7 fd186907  |2 czenas 
655 9 |a electronic books  |2 eczenas 
700 1 |a Stein, Manuel. 
700 1 |a Libove, Charles. 
710 2 |a Langley Aeronautical Laboratory. 
710 1 |a United States.  |b National Advisory Committee for Aeronautics. 
776 0 8 |i Print version:  |a Batdorf, S.B.  |t Critical combinations of longitudinal and transverse direct stress for an infinitely long flat plate with edges elastically restrained against rotation.  |d Langley Field, VA : Langley Memorial Aeronautical Laboratory, 1946  |w (OCoLC)71843726 
830 0 |a NACA collection. 
856 4 0 |u https://proxy.k.utb.cz/login?url=https://app.knovel.com/hotlink/toc/id:kpCCLTDSI2/critical-combinations-of?kpromoter=marc  |y Full text