Description of stress-strain curves by three parameters

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Bibliographic Details
Main Author Ramberg, Walter
Corporate Author United States. National Advisory Committee for Aeronautics
Other Authors Osgood, William R.
Format Electronic eBook
LanguageEnglish
Published Washington D.C. : National Advisory Committee for Aeronautics, 1943.
SeriesTechnical note (United States. National Advisory Committee for Aeronautics) ; no. 902.
Subjects
Online AccessFull text
ISBN9781680156034
1680156039
Physical Description1 online resource (13, [15] pages) : illustrations

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Abstract:A simple formula is suggested for describing the stress-strain curve in terms of three parameters: namely, Young's modulus and two secant yield strengths. Dimensionless charts are derived from this formula for determining the stress-strain curve, the tangent modulus, and the reduced modulus of a material for which these three parameters are given. Comparison with the tensile and compressive data on aluminum alloy, stainless-steel, and carbon-steel sheet in NACA Technical Note No. 840 indicates that the formula is adequate for most of these materials. The formula does not describe the behavior of alclade sheet, which shows a marked change in slope at low stress. It seems probable that more than three parameters will be necessary to represent such stress-strain curves adequately.
Item Description:"July 1943."
NACA TN no. 902.
Bibliography:Includes bibliographical references.
ISBN:9781680156034
1680156039
Access:Plný text je dostupný pouze z IP adres počítačů Univerzity Tomáše Bati ve Zlíně nebo vzdáleným přístupem pro zaměstnance a studenty
Physical Description:1 online resource (13, [15] pages) : illustrations