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

• 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
• Language: English
• Published: Langley Field, VA : Langley Memorial Aeronautical Laboratory, 1946.
• Series: NACA collection.
• Subjects: Airplanes > Design and construction.; Aerodynamics > Research.; elektronické knihy; electronic books
• ISBN: 9781680156522; 1680156527
• Physical Description: 1 online resource (14, [6] pages)
• Item Description: "Report no. L-49."; "Originally issued March 1946 as Advance Restricted Report L6A05a."; "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."
• Access: Plný text je dostupný pouze z IP adres počítačů Univerzity Tomáše Bati ve Zlíně nebo vzdáleným přístupem pro zaměstnance a studenty

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.