Flexure Testing of Glass Fibers
in Materials Testing Laboratory at the University of Missouri-Rolla
Photos by Jeff Thomas, January 18, 2000.

 

Click on value for raw data and load-deflection curve.

  Flexure Modulus (GPa)
NAP-3 Silica Silica McDo F43 Silica K Old
Sample 1 45.69* 71.60* 72.99 77.07 87.45
2 68.50 77.23 75.74 79.89 88.71
3 56.41 79.13 74.99 65.52 88.69
4 67.22 78.35 75.80 68.71 91.15
5 62.97 79.35 73.88 70.19 91.00
6 58.75 79.52   73.55 91.89
7       65.72 88.98
8       67.27  
9          
10          
Average   62.77 78.72 74.68 70.99 89.70
STD   4.68 0.84 1.09 5.00 1.52
* Eliminated from average due to improper span measurement

Click on image to enlarge.

Derivation of E

From beam deflection theory for 3-point bending,

y = x(3L2 - 4x2)P / 48EINA

where

y = deflection of middle of beam (read by Instron 4469 UTM)
x  = L / 2
L = span
P = load (read in grams using gram-scale)
E = flexure modulus
INA = moment of inertia about the neutral axis = pr4 / 4 (for cylindrical samples)

Rearranging,

E = (P/y)L3  / 12pr4

where

P/y = slope of load-deflection curve

For unit conversions in this particular case, multiply by "9.81(1000)/25.4", because the load is measured in grams, the deflection is measured in inches, the radius is measured in millimeters, and we desire Pascals as the units for E.