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130901s1946 vauad obt f000 0 eng d |
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|a OCLCE
|b eng
|e pn
|c OCLCE
|d OCLCQ
|d OCLCF
|d SINTU
|d KNOVL
|d ZCU
|d OCLCQ
|d UAB
|d OCLCQ
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|d YOU
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|d OCLCO
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|a 914554333
|a 951667684
|a 977336518
|a 987147222
|a 1047748312
|a 1229063615
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|a 9781680156522
|q (electronic bk.)
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|a 1680156527
|q (electronic bk.)
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|a (OCoLC)857368708
|z (OCoLC)914554333
|z (OCoLC)951667684
|z (OCoLC)977336518
|z (OCoLC)987147222
|z (OCoLC)1047748312
|z (OCoLC)1229063615
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|a TL671.2
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|a 629.1341
|2 23
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|a UAMI
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|a Batdorf, S. B.
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|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.
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|a NACA wartime reports
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|a Langley Field, VA :
|b Langley Memorial Aeronautical Laboratory,
|c 1946.
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|a 1 online resource (14, [6] pages)
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|a text
|b txt
|2 rdacontent
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|a computer
|b c
|2 rdamedia
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|a online resource
|b cr
|2 rdacarrier
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|a "Report no. L-49."
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|a "Originally issued March 1946 as Advance Restricted Report L6A05a."
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|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."
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|a Includes bibliographical references (page 13).
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|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.
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|3 Use copy
|f Restrictions unspecified
|2 star
|5 MiAaHDL
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|a Electronic reproduction.
|b [Place of publication not identified] :
|c HathiTrust Digital Library,
|d 2013.
|5 MiAaHDL
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|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
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|a digitized
|c 2013
|h HathiTrust Digital Library
|l committed to preserve
|2 pda
|5 MiAaHDL
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|a Print version record.
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|a Access restricted to Ryerson students, faculty and staff.
|5 CaOTR
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|a Knovel
|b ACADEMIC - Aerospace & Radar Technology
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|a Airplanes
|x Design and construction.
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|a Aerodynamics
|x Research.
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|a Avions
|x Conception et construction.
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|a Aérodynamique
|x Recherche.
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|a Aerodynamics
|x Research
|2 fast
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|a Airplanes
|x Design and construction
|2 fast
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|a Stein, Manuel.
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|a Libove, Charles.
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|a Langley Aeronautical Laboratory.
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|a United States.
|b National Advisory Committee for Aeronautics.
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|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
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|a NACA collection.
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|u https://appknovel.uam.elogim.com/kn/resources/kpCCLTDSI2/toc
|z Texto completo
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|a 92
|b IZTAP
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