Tensile Test and Strength Analysis of Plastic and Brittle Female Thread

2021 ◽  
Vol 20 (0) ◽  
pp. 118-124
Author(s):  
Ryuta Kitamura ◽  
Kaito Osada ◽  
Atsushi Wada ◽  
Atsushi Takano
Keyword(s):  
Tensile Test ◽  
Strength Analysis

scholarly journals Mechanical Properties of Welded Joints of 1.3964 Steel for Computer Aided Engineering (CAE) Purposes

2020 ◽  
Vol 220-221 (1-2) ◽  
pp. 15-28
Author(s):  
Radosław Kiciński ◽  
Wojciech Jurczak
Keyword(s):  
Mechanical Properties ◽  
Tensile Test ◽  
Welded Joints ◽  
Material Model ◽  
Computer Aided Engineering ◽  
Strength Analysis ◽  
Welded Steel ◽  
Static Tensile Test ◽  
Computer Aided ◽  
Static Tensile

AbstractThe article presents the study of mechanical properties of welded steel from which the hull of a modern mine destroyer was made. Keeping the tightness of ship compartments during operation depends on the strength of these joints. The results of testing the mechanical properties of 1.3964 steel and its welded joints subjected to a static tensile test were presented, and a Johnson – Cook material model was proposed. The material model can be used in CAE (Computer Aided Engineering) simulations related to hull strength analysis.

What Is Right? A Character-Strength Analysis

2009 ◽  
Author(s):  
Linda L. Moore ◽  
Daniel J. Van Ingen
Keyword(s):  
Strength Analysis ◽  
Character Strength

Influence of residual stresses in the tensile test of cold drawn wires

10.1617/13917 ◽  
2003 ◽  
Vol 36 (262) ◽  
pp. 548-552 ◽  
Author(s):  
J. M. Atienza
Keyword(s):  
Residual Stresses ◽  
Tensile Test

Tensile test of sintered Si3N4 and the influence of process defects such as pores on fracture strength.

1989 ◽  
Vol 38 (424) ◽  
pp. 32-38 ◽  
Author(s):  
Hidehiro KISHIMOTO ◽  
Akira UENO ◽  
Hiroshi KAWAMOTO ◽  
Sachio URA
Keyword(s):  
Tensile Test ◽  
Fracture Strength

Validation of Numerical Models Used for Designing the Composite Blade for ILX-27 Rotorcraft

2019 ◽  
Vol 2019 (4) ◽  
pp. 23-31
Author(s):  
Jakub Wilk ◽  
Radosław Guzikowski
Keyword(s):  
Epoxy Composite ◽  
Numerical Models ◽  
Experimental Studies ◽  
Strength Analysis ◽  
Laminate Glass ◽  
Composite Blade ◽  
Real Objects ◽  
Validation Procedure ◽  
Research Objects ◽  
Comparison Of The Results

Abstract The paper presents the validation procedure of the model used in the analysis of the composite blade for the rotor of the ILX-27 rotorcraft, designed and manufactured in the Institute of Aviation, by means of numerical analyses and tests of composite elements. Numerical analysis using finite element method and experimental studies of three research objects made of basic materials comprising the blade structure – carbon-epoxy laminate, glass-epoxy composite made of roving and foam filler – were carried out. The elements were in the form of four-point bent beams, and for comparison of the results the deflection arrow values in the middle of the beam and axial deformations on the upper and lower surfaces were selected. The procedure allowed to adjust the discrete model to real objects and to verify and correct the material data used in the strength analysis of the designed blade.

COMPRESSIVE STRENGTH ANALYSIS ON PROBLEMATIC SOILS STABILIZED WITH FLY ASH IN JORDAN

2018 ◽  
Vol 17 (8) ◽  
pp. 1855-1861
Author(s):  
Nicolae Taranu ◽  
Monther Abdelhadi ◽  
Ancuta Rotaru ◽  
Maria Gavrilescu
Keyword(s):  
Compressive Strength ◽  
Fly Ash ◽  
Strength Analysis ◽  
Problematic Soils
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