Difference between revisions of "R3DC Report 2-08"
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| Line 12: | Line 12: | ||
|Material || Youngs Modulus|| Density | |Material || Youngs Modulus|| Density | ||
|- | |- | ||
| − | | Hexacell|| | + | | || <math>\frac{N}{mm^2}</math>|| <math>\frac{kg}{mm^3}</math> |
| + | |- | ||
| + | | Hexacell|| <math>1.4 \times 10^5</math> || <math>2.4 \times 10^7</math> | ||
|- | |- | ||
| Hexacell with holes|| || | | Hexacell with holes|| || | ||
|- | |- | ||
| − | | Carbon Fiber Rods|| | + | | Carbon Fiber Rods|| <math>2.1 \times 10^5</math> || <math>5.8 \times 10^7</math> |
|} | |} | ||
Revision as of 03:33, 7 February 2008
Introduction
Geometry
Basic Sizes
Material Specifications
Specific part Drawings
Endplate Deflection
Point Load Deflection
| Material | Youngs Modulus | Density |
| Hexacell | ||
| Hexacell with holes | ||
| Carbon Fiber Rods |
Distributed Load Deflection
Distributed load FEA
Carbon Rod Buckling
Compression
Buckling Load Threshold
Buckling FEA
=3-D Analysis