Strength analysis of intraosseous wire fixation for avulsion fractures of the fifth metatarsal base

2004 ◽  
Vol 43 (4) ◽  
pp. 225-230 ◽  
Author(s):  
Anthony R Giordano ◽  
Lawrence M Fallat
Keyword(s):  
Strength Analysis ◽  
Avulsion Fractures ◽  
Wire Fixation

scholarly journals Motion and Strength Analysis of 2-Tine Staple and K-Wire Fixation in Scapholunate Ligament Stabilization in a Cadaver Model

2021 ◽  
Vol 3 (2) ◽  
pp. 67-73
Author(s):  
Daniel Hess ◽  
Anthony Archual ◽  
Zachary Burnett ◽  
Hans Prakash ◽  
Emily Dooley ◽  
...  
Keyword(s):  
Strength Analysis ◽  
Scapholunate Ligament ◽  
Wire Fixation

Tension Wire Fixation of Avulsion Fractures in the Hand

1987 ◽  
Vol &NA; (214) ◽  
pp. 113???120 ◽  
Author(s):  
Jesse B. Jupiter ◽  
Joseph E. Sheppard
Keyword(s):  
Avulsion Fractures ◽  
Wire Fixation ◽  
Tension Wire

What Is Right? A Character-Strength Analysis

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

Wire fixation versus rigid titanium plate after sternotomy – Results of a randomized, prospective, multi-center trial

2012 ◽  
Vol 60 (S 01) ◽  
Author(s):  
S Lehmann ◽  
MS Wong ◽  
K Zehr ◽  
BJ DeGuzman ◽  
HE Garrett ◽  
...  
Keyword(s):  
Titanium Plate ◽  
Wire Fixation

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.

Sign in / Sign up

Export Citation Format

Share Document