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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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Detalles Bibliográficos
Clasificación:Libro Electrónico
Autor principal: Batdorf, S. B.
Autores Corporativos: Langley Aeronautical Laboratory, United States. National Advisory Committee for Aeronautics
Otros Autores: Stein, Manuel, Libove, Charles
Formato: Electrónico eBook
Idioma:Inglés
Publicado: Langley Field, VA : Langley Memorial Aeronautical Laboratory, 1946.
Colección:NACA collection.
Temas:
Acceso en línea:Texto completo

MARC

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008 130901s1946 vauad obt f000 0 eng d
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029 1 |a GBVCP  |b 856590681 
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 
050 4 |a TL671.2 
082 0 4 |a 629.1341  |2 23 
049 |a UAMI 
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). 
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. 
506 |3 Use copy  |f Restrictions unspecified  |2 star  |5 MiAaHDL 
533 |a Electronic reproduction.  |b [Place of publication not identified] :  |c HathiTrust Digital Library,  |d 2013.  |5 MiAaHDL 
538 |a Master and use copy. Digital master created according to Benchmark for Faithful Digital Reproductions of Monographs and Serials, Version 1. Digital Library Federation, December 2002.  |u http://purl.oclc.org/DLF/benchrepro0212  |5 MiAaHDL 
583 1 |a digitized  |c 2013  |h HathiTrust Digital Library  |l committed to preserve  |2 pda  |5 MiAaHDL 
588 0 |a Print version record. 
506 |a Access restricted to Ryerson students, faculty and staff.  |5 CaOTR 
590 |a Knovel  |b ACADEMIC - Aerospace & Radar Technology 
650 0 |a Airplanes  |x Design and construction. 
650 0 |a Aerodynamics  |x Research. 
650 6 |a Avions  |x Conception et construction. 
650 6 |a Aérodynamique  |x Recherche. 
650 7 |a Aerodynamics  |x Research  |2 fast 
650 7 |a Airplanes  |x Design and construction  |2 fast 
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://appknovel.uam.elogim.com/kn/resources/kpCCLTDSI2/toc  |z Texto completo 
994 |a 92  |b IZTAP