Theoretical prediction of dynamic composite material properties for hypervelocity impact simulations

2009 ◽  
Vol 36 (7) ◽  
pp. 899-912 ◽  
Author(s):  
S. Ryan ◽  
M. Wicklein ◽  
A. Mouritz ◽  
W. Riedel ◽  
F. Schäfer ◽  
...  
Keyword(s):  
Composite Material ◽  
Theoretical Prediction ◽  
Material Properties ◽  
Hypervelocity Impact ◽  
Impact Simulations

Sensitivity of hypervelocity impact simulations to equation of State

1987 ◽  
Vol 5 (1-4) ◽  
pp. 333-341 ◽  
Author(s):  
Kathleen S. Holian ◽  
Michael W. Burkett
Keyword(s):  
Equation Of State ◽  
Hypervelocity Impact ◽  
Impact Simulations

Influence of Rubber Particle Size on Functional Properties of a Composite Material Based on Scrap Tires and a Polymer Binder

2020 ◽  
Vol 850 ◽  
pp. 107-111
Author(s):  
Laimonis Mālers ◽  
Agnija Cirvele
Keyword(s):  
Particle Size ◽  
Composite Material ◽  
Functional Properties ◽  
Material Properties ◽  
Rubber Particle ◽  
Polymer Binder ◽  
Scrap Tires ◽  
Elongation At Break ◽  
Rubber Particles ◽  
Purposeful Selection

Functional properties of composite material based on mechanically grinded scrap tires with different particle size of fractioned crumb and polyurethane type polymer binder were investigated to estimate influence of rubber particles size and content on composite material properties (Shore C hardness, compressive stress at 10 % deformation, tensile strength, elastic modulus and elongation at break, apparent density). Optimization possibilities of composite material consisting of rubber particles with different sizes or fractions were investigated. The obtained results show that variation of composition of the composite material by changing size of rubber granulate have definite influence on selected properties of the material. Purposeful selection and mutual combination of rubber particles size included in material can ensure desirable and predictable mechanical properties of composite material.

RETRACTED: The laser-driven flyer system for space debris hypervelocity impact simulations

2009 ◽  
Vol 267 (18) ◽  
pp. 3252-3257 ◽  
Author(s):  
Gong Zizheng ◽  
Dai Fu ◽  
Cao Yan ◽  
Zhang Wenbing ◽  
Yang Jiyun ◽  
...  
Keyword(s):  
Space Debris ◽  
Hypervelocity Impact ◽  
Impact Simulations

scholarly journals Advanced Composite Fan Blade Flight Evaluation Program

1976 ◽  
Author(s):  
M. H. Chopin
Keyword(s):  
Composite Material ◽  
Air Force ◽  
Material Properties ◽  
Metal Matrix ◽  
Matrix Composites ◽  
Basic Design ◽  
Turbine Engine ◽  
Advanced Composite ◽  
Advanced Composite Materials ◽  
Fan Blade

The preparation for and conduct of the first flight by the U. S. Air Force of a turbine engine fan stage fabricated of advanced composite materials is discussed. Composite material properties and basic design philosophy is presented along with preliminary flight evaluation results. This is the first application of filamentary-reinforced metal matrix composites to a turbine engine structural component.

Limits on Unidirectional Composite Material Properties

1969 ◽  
Vol 3 (4) ◽  
pp. 728-731
Author(s):  
H.E. Brandmaier
Keyword(s):  
Composite Material ◽  
Material Properties ◽  
Unidirectional Composite ◽  
Unidirectional Composite Material

Experimental Characterization of Composite Material Properties

2017 ◽  
pp. 227-237
Author(s):  
P. Yukhymets ◽  
R. I. Dmytriienko ◽  
I. Ramadan ◽  
S. N. Bukharov
Keyword(s):  
Composite Material ◽  
Material Properties ◽  
Experimental Characterization

A CRASHWORTHINESS SIMULATION FOR A LIGHT AIRCRAFT CONSTRUCTED OF COMPOSITE MATERIALS

2015 ◽  
Vol 39 (4) ◽  
pp. 829-843 ◽  
Author(s):  
Pu-Woei Chen ◽  
Kuan-Jung Chen
Keyword(s):  
Composite Material ◽  
Aluminum Alloy ◽  
Composite Materials ◽  
Fiber Composite ◽  
Impact Angle ◽  
The Finite Element Method ◽  
Dynamic Impact ◽  
Carbon Fiber Composite ◽  
Impact Speed ◽  
Impact Simulations

This study analyzes the crashworthiness of a light aircraft that is constructed from composite materials. The finite element method is employed to conduct dynamic impact simulations on carbon fiber composite fuselages. The results show that the safe impact speed for an aluminum alloy cockpit crashed at a 30° impact angle is 9.59 m/s, but a cockpit made of composite material can withstand a speed greater than 18.05 m/s. The safe impact angle for an aluminum alloy cockpit is 16.56°, but that for a composite cockpit is 84.9°. The safety crash zone for a composite material cockpit is 160% greater than that for an aluminum alloy cockpit.

Multi-layer insulation material models suitable for hypervelocity impact simulations

2008 ◽  
Vol 35 (12) ◽  
pp. 1853-1860 ◽  
Author(s):  
D.M. White ◽  
M. Wicklein ◽  
R.A. Clegg ◽  
H. Nahme
Keyword(s):  
Hypervelocity Impact ◽  
Insulation Material ◽  
Material Models ◽  
Impact Simulations
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