GRAPHITE EPOXY COMIPOSITES
BY MEASURING THEIR ELECTRICAL RESISTANCE
by
Avraham Benatar
zz
SUBMITTED IN PARTIAL FULFILLMENT OF THE REQUIREMENTS FOR THE
DEGREE OF
BACHELOR OF SCIENCE IN MECHANICAL-ENGINEERING
at the
MASSACHUSETTS INSTITUTE OF TECHNOLOGY May, 1981.
GIMassachusetts
Institute of TechnologySignature Certified of Autho ... Department I by.. . .. . . of Mech-anical Engineering May, 1981 Nam P. Suh Thesis Supervisor A c p t e .-
~~~~~~~~~.
. . .. ~ ~~// .rmen, Department Committee MASSACHUSETTS INST1i'UT'E OF Tlr.'OTLOGV -JUL '7 1981 LIBRARIS ,/
1981
AcceptedGRAPHITE EPOXY COMPOSITES
BY MEASURING THEIR ELECTRICAL RESISTANCE
by
Avraham Benatar
Submitted to the Department of Mechanical Engineering on May 13, 1981 in partial fulfillment of the requirements for the Degree Bachelor of Science in
Mechanical Engineering
ABSTRACT
The moisture content of graphite epoxy composites can be used to determine the amount of degradation suffered by the material due to exposure to humidity environments. The common method used to measure the moisture content of these composites is to weigh them; this is sometimes undesirable or impossible. Therefore, a change in another property which depends on the moisture concentration, overall resistance, may be measured; this can then be used to determine the moisture concentration.
Unidirectional and multidirectional graphite epoxy composites were exposed to high temperature and high humidity (100% RH) environments. Their weight and electrical resistance were measured. It was found that for both composites the resistance across the length was
independent of the moisture content. For the unidirectional composites the normalized change in resistance across the width was found to be proportional to moisture concentration squared. For multidirectional composites the resistance across the thickness was measured in three different ways. The four terminal resistance measurment method was most effective because it minimized the contact resistance. For multidirectional composites the normalized change in resistance across the thickness was found to be proportional to the moisure concentration.
Thesis Supervisor: Dr. Nam P. Suh
AC KNOWLE DGEMENTS
First, I would like to thank Professor Nam Suh for his guidance, and for sharing his time and wisdom with me. My thanks to Dr. Tim Gutoski for many stimulating discussions, and for his many helpful suggestions.
This project was sponsored by The Boeing Company. My thanks to Mr. Alan Taylor for his helpful comments. I would also like to thank Dr. Duk Kim for preparing the multidirectional composites, and the TELAC group at M.I.T.
for making the unidirectional composites.
I am obliged to many people in the Laboratory for Manufacturing and Productivity at M.I.T. I would like to express my appreciation to Fred Anderson, Fred Cote, Bob Crane, Michael Demaree, John Ford, and Ralph Whittemore; these lab technicians and instructors helped in the preparation of samples and instrumentation.
My thanks to my office mates - Richard Okine, Byung Kim, Myung Moon, Frank Waldman, and Teeraboon Intragumtornchai.
I am deeply indebted to Joy David for her constant support, and for her enormous help in typing this thesis. Most of all, many thanks to my family, especially Dad and Mom, for their everlasting support, love, encouragement, and dedication to education.
TABLE OF CONTNETS Section Page ABSTRACT 2 ACKNOWLE DGM ENTS 3 TABLE OF CONTENTS 4 LIST OF ILLUSTRATIONS 5 LIST OF TABLES 6 I. INTRODUCTION 7 A. Background 7 B. Theory 10
II. EXPERIMENTAL PROCEDURES 17
A. Unidirectional Composites 17 B. Multidirectional Composites 17
III. RESULTS AND DISCUSSION 23
.A. Unidirectional Composites 23
B. Multidirectional Composites 23
IV. CONCLUSIONS AND RECOMMENDATIONS 32 Appendices
A. STATISTICAL SUMMARY OF THE EXPERIMENTAL
RESULTS 34
B. MOISTURE ABSORPTION BY COMPOSITES 37
LIST OF ILLUSTRATIONS
Figure Page
1. Unidirectional Composite With Longitudenal
Fibers 9
2. A Reperesentative Volume Element of a
Unidirectional Composite 11
3. Multidirectional Composite 14
4. Resistance Measurements of The Unidirectional
Samples 18
5. Resistance Measurements of The Multidirectional
Samples Using Methods 1 and 2 20 6. Jig For Modified Four Terminal Resistance
Measurement of The Multidirectional Samples 21 7. Standard Four Terminal Resistance Measurement
of a Wire 22
8. Change in Resistance Measured Across The Length
of The Unidirectional Samples Due to Moisture 24 9. Normalized Change in Resistance Across The
Width of The Unidirectional Samples Due to
Moisture 25
10. Change in Resistance Measured Across The Length of The Multidirectional Samples Due to Moisture
(Measurement Method 2) 26
11. Change in Resistance Across The Thickness (Measured Using Method 1) of The
Multidirectional Samples Due to Moisture 28 12. Change in Resistance Across The Thickness
(Using Method 2) of The Multidirectional
Samples Due to Moisture 29
13. Change in Resistance Across The Thickness (Using Method 3) of The Multidirectional
Samples Due to Moisture 31
14. Description of The Boundry Conditions Used in
The Solution of Fick's Equation 38
5.
;-P-:>isor-vt i A
msortion
D :n Values ForLIST OF TABLES
Table Page
1. Typical Hygrothermal Properties of
Unidirectional Graphite Epoxy Composites 16 2. Resistance Measurement Across The Length of
The Unidirectional Samples 34
3. Change in Resistance Across The Width of The
Unidirectional Samples 34
4. Resistance Measurement (Method 2) Across The
Length of The Multidirectional Samples 35 5. Change in Resistance (Measurement Method 1)
Across The Thickness of The Multidirectional
Samples 35
6. Change in Resistance (Measurement Method 2) Across The Thickness of The Multidirectional
Samples 35
7. Change in Resistance (Measurement Method 3) Across The Thickness of The Multidirectional
I. INTRODUCTION
A. Background
The use of graphite epoxy composites is rapidly growing, especially in the aerospace industry. While in use, these composites are often exposed to diverse environmental conditions; specifically, they are exposed to different temperature and humidity environments which affect their mechanical properties. It was found that the moisture content of these composites is related to the change in their mechanical and physical properties [1]. Therefore, it is necessary to accurately determine the moisture content of these composites.
The most common technique used to monitor the moisture content in composites is by monitoring the weight of the samples. However, this technique is not effective when the sample is in a stress loading jig or in operation on an airplane. Weighing samples that are in operation requires isolating them from the integral systems; this is not always possible. In addition, these samples collect residues such as those produced by the corrosion of the loading jigs or chemicals from the environment. Weighing them and assuming that the change in weight is due only to moisture can lead to erroneous results. Therefore, moisture measurement should be done indirectly by measuring another material property that is affected by moisture but is easier to measure. One such property is the overall resistance of the composite.
The overall resistance of a graphite epoxy composite is due to the contact resistance between touching fibers [2] and to the number of contact points. Moisture in the composite causes swelling of. the matrix. The swelling causes the fibers to separate slightly; this increases the contact resistance and may even lead to a complete loss of contact at some points. The increase in the contact resistance and the decrease in the number of contact points causes the overall resistance of the composite to increase.
For a unidirectional composite with fibers aligned to the length (see Figure 1), the swelling affects the width and the thickness of the composite. The effect of moisture (swelling) on the length is negligible because it is constrained by the stiff graphite fibers. Belani and Broutman [2] correlated the moisture content of graphite epoxy composites to the change in their electrical resistance. They found the following correlation:
bWere R(t)
Where
AR_ Wet resistance-Dry resistance
R Dry resistance
AW Wet weight-Dry weight W Dry weight
It is important to note, here, that even though the increase in thickness increases the cross sectional area through which the resistance is measured (and thus, the resistance
rs.i.anc eh'
:in:craes.
-Thisis o
'
he:
i-:.s dtn.atthte
f ctt'
resistance
increases.
This
is
due to the fact that the
t
_"'V
b--
...-Ie
=
IFigure 1. Unidirectional Composites diih Longitudinal Fibers
7
-4-~~~~~~~~~~~
.e ,."..~~~~~~~~~~~~~~~·~*
matrix has a much higher resistance than the fibers.
B. Theory
The governing factor on the overall resistance of graphite epoxy composites is the contact resistance between the touching fibers. In general the contact resistance between two solids is the sum of the constriction resistance and the film resistance. The constriction resistance is due to the two solids having contact only at some points, because of the surface roughness. Thus, the area through which the current flow passes is less than the apparent
contact area. The film resistance is due to the two solids being separated at some points by a thin layer of a third
material which has a higher resistivity.
Graphite fibers have a very chemically reactive surface. So in general they would form a surface layer which will act as a film when they come in contact. In addition, most fiber and prepreg manufacturers coat graphite fibers with an epoxy compatible sizing (usually some epoxy monomer) for better bonding to the matrix. Therefore, in the composite the fibers will be separated by a thin film, which is usually epoxy (see Figure 2). Since the fibers do not actually contact each other, the constriction resistance has little, if any, affect on the contact resistance; the contact resistance is governed by the film resistance.
Figure 2. A Representative Volume Element of a Unidirectional Comorosite -*-·- ·i? - -.. b a-· ;r c -'d ·' ·· L3 -··-VI -· ---r ·. _··n-- ·-:··Z "-r.- --- · · · ·-; -·-·
I'Cti
1Icl F I F
' '
-';-i r i -t J · ru 1 i-rUr r I r Y ;·:?s .c -' -"The film resistance between two materials being separated by a third is given by the following relation[3]:
·
P _S (2)
f
A,
Where
Rf= film resistance,
f= resistivity of film material, cm S = film thickness, cm
AC= area of contact, cm
As explained above, most fibers throughout the composites, as those in Figure 2, will be separated by a thin film, probably made of epoxy. Swelling of this film due to moisture will increase its thickness, thereby increasing the
film resistance. The resistivity and area of contact will remaine approximately the same, because the moisture concentration in the matrix is small (less than 8%).
Tsai and Hahn[4] show that the dilatation strain is linearly related to the moisture concentration. The change in the film thickness is linearly related to the dilatation strain. And the change in the film thickness is proportional to the film resistance. Therefore, for unidirectional composites, which swell in their thickness and their width, the following correlation is expected:
AR a (At) (b) (3)
where At (the change in thickness) and b (the change in width) vary linearly with the moisture content. Therefore,
R
and normalizing gives
~rR d /awl~ (5) R
where R and W are constants. This is in agreement with correlation found by Belani and Broutman [23.
Similarly, for multidirectional composites only thickness will be affected by moisture. (See Figure 3.) length and width of the composite will be constrained by fiber. Thus, the following correlation is expected:
AR t (6)
And the change in thickness is linearly proportional to change in the moisture content. Thus,
AR X W (7) normalizing, %R ( '6W (8) R W the the The the the
It is important to remember that since the strains are linearly proportional to the change in resistance, then any strain applied on the sample will also cause a change in resistance. Therefore, changes in the stresses applied to the samples will cause changes in the resistance. The change in resistance due to stress may be subtracted from the change in total resistance (resistance due to stress plus resistance due to moisture) in cases where stress
strain relations are linear.
Due to thermal expansion, temperature changes also cause changes in the strains. Tsai and Hahn [4] give typical values for te coefficient of therial expansion, >Lei, and the swelling coefficient, i, for unidirectional
1
4-Figure 3.
M':vultidirectional
__ :_
composites. (See Table 1.) They suggest the following linear relations:
Js ~~~~=diOfA~ ~(9)
where
= thermal strain in the i direction AT = change in temperature,
6'= swelling strain in the i direction
c = moisture concentration
Using these relations, these typical values in the transverse directions for a moisture concentration, c=0.005 and the temperature change, T=10C, and typical values for
It andS2 from Table 1 gives,
6
~~TEl
67~~(]0)
This means that for some typical temperature changes between measurements (10°C) and some typical moisture content (0.5%), the thermal strain is only about 10% of the swelling strain. Thus, in most applications, the thermal strain may be neglected. For higher temperature variations, the thermal strain may be subtracted by assuming the (above) linear relation without substantial errors.
Typical Hygrothermal Propnerties of Un ireti ri-.a Graphite Epoxy Cormoposites
(Taken
Fro-,
.eferene
4')
P C }>x KiT y KTz ox ay ) 'z g/cmr3 Jl(g-K) W/(m-K) W/(m K) (pmlnm)K (pm/m)/K 1.6 1.0 4.62 0.72 -0.3 28.1 a b KH Ea/R Py z mm2/s K m/m m/m 0.018 I 6.51 5722 0 0.44 TO to OC 177 ,_ · : . .:- - , , z __ I - -_ - ___ -r -- --- ·- ·-·---- -- ·- --- --- ·---- --- -- --- ---... ";'.-, :: ---..-.. .-I--I-···-. - ----c---.. .. .', .2 ·
II. EXPERIMENTAL PROCEDURES
A. Unidirectional Composites
Unidirectional graphite epoxy composites were prepared by the Technology Laboratory for Advanced Composites (TELAC) in the Department of Aeronautics and Astronautics at the Massachusetts Institute of Technology. Five samples were cut from these 0.015 inch thick composites; the dimensions were 3/4" by 2". The changes weight and electrical resistance of these samples were measured after exposure (for different periods of time) to a 100% RH (relative humidity) and 1000C environment. The weight and resistance were measured after the samples were cooled to room temperature. As shown in Figure 4, both the longitudenal and the transverse resistances were measured using a Hewlett Packard digital multimeter. Because the samples were thin, the ends could not be effectively coated with the conductive silver paint. Therefore, the resistance measurement was done by just touching the probes against the ends, without applying any pressure.
B. Multidirectional Composites
Multidirectional composites 1/4" thick were prepared by Boeing Aircraft Company. Five samples (again 3/4" by 2") were cut from these composites. The weight and resistance changes were measured after the samples were placed (for
Figure 4.
Resistance Measurements of the
different lengths of time) in a pressure cooker filled with water. By using the pressure cooker, it was possible to
expose the samples to both a high temperature (1210C) and a high humidity (100% RH) environment.
Three different methods were used to measure the electical resistance of the samples across the width and the thickness. In all of the methods, Hewlett Packard digital multimeters were used.
The first method was to file the surface where, the probes were going to placed, to expose some of the fibers and then to coat the surface with conductive silver paint. (See Figure 5.) This was done to minimize the fluctuations in the resistance measurement.
The second method was a modification of the first. After each exposure to the high temperature/high humidity environment, the old silver paint was removed and replaced with a new coat. This eliminated any effects of the moisture on the interface between the surface and the silver paint. (Note - This procedure was used on four samples with dimensions of 3/16" by 3/4" by 2".)
The final procedure used the four terminals method of --resistance measurement. Figure 6 shows the jig which was constructed to perform these measurements. Because the samples were quite thin, it was not possible to measure the electrical potential between two points on the thickness. (See Figure 7.) Therefore, it was assumed that the surfaces formed two equipotential sheets. Then the potential between the two surfaces was measured.
Areas Coated ,ith Conductive
Silver Paint
Figure 5.
Resistance Measurements of the
Multidirectional Composites Using
SAt MLE
.,
"'. ::..
.J,,;
.-.:, ., .
r1I
Jig For odified Four Terminal Resistance
1
_
-q_
II " I~, , fI -- .. II - _ , -. -I -' .'. - · - : C, ·~
Figure 6.,
'I
A
Figure
7.
Standard Four Terminal ResistanceIII. RESULTS AND DISCUSSIONS
A. Unidirectional Composites
Figure 8 shows the electrical resistance measured across the length of the samples as a function of moisture content. As expected, this resistance is independent of the moisture concentration because it measures the resistance of the fibers; it is not affected by matrix swelling or moisture at the interface. The value of the resistance is high due to the high contact resistance. Having a thicker sample and coating its end with conductive silver paint would reduce the contact resistance substantially.
Figure 9 shows the normalized change in resistance measured across the width of the sample as a function of moisture content. The results are in agreement with the correlation discussed in Section I. It is important to note that the fluctuation in the resistance between samples was very high; this was probably the combined result of the rough method of measurement, the lack of conductive silver paint, and the non-uniformity between the samples.
B. Multidirectional Composites
Figure 10 shows the electrical resistance measured across the length of the samples as a function of the moisture content. As with the unidirectional composites, the resistance across the length is not affected by the matrix swelling or the moisture at the fiber-matrix interface.
2.0
3,0 I Resistance (ohms)Figure 8. Change
in Resistance
,.easured
Across
the Lerth,
of the Unidirectional samples Due to :i->oisture0 c) .4 O a) 0 1.0 . 0 1.0 e -, ____1 _ __ __ _I_ I I · _- r · _· · -, ~ ~ ~ ~ - ~ ~ ~ ~ ~ ~
-I -.0
c--
t-I -
--
O
---
r
I I I " 4.0 'Resistance Chanige,
(
)
Figure 9. Normalized Change in Resistance Across the
Width o the Unidirectional marpltes 2ue to
Moisture
c) 0) CD 4~ 0 .r5
FtO--o
i /1i
I k3" 1
.1 .2
Resistance (ohms)
Figure 10. Change in Resistance PMeasured Across the Length of the 2.^ultidirectional Snples Due to oisture (Measurement ethod 2)
., 75 4-+) 0do 0 .50 +: ., .25 _ ___ _
The resistance across the thickness of the samples was measured using the three different methods described in Section II. The normalized change in resistance, as it was
measured by the first method, is presented in Figure 11 as a
function of moisture content. In this case, the line that best fits the data does not go through the (0,0) point; it is shifted to the right. This is probably the result of the moisture environment affecting the interface between the surface and the conductive silver paint. When the samples were exposed to humidity at a high temperature, the silver paint tended to debond from the surface. This increased the contact resistance, thus making it a function of the time that the samples were exposed to humidity. The increase in the contact resistance between the conductive silver paint and the surface caused the (above-mentioned) shift to the
right.
To minimize the effect of moisture on the contact resistance, the silver paint was replaced before each measurement. (See method 2 as described in Section II.) As shown in Figure 12, this procedure gave the correlation predicted in Section I. The normalized change in resistance across the thickness was found to be linearly proportional to the moisture content. However, it should be remembered that a contact resistance still existed, and it may have been significant. The contact resistance may create difficulties in the practical application of this this procedure.
5
Resistance Change,
4AB
Ri
Figure 11.
Change in Resistance Across the Thickness(Measured Using ?,ethod 1) of the ;iultidirectional Samples Due to ioisture
.3
+I)
r.
0 0 a) s-f .1 / / I I .0 / IResistance Change,
aR
RFigure 12. Change in Resistance Across the Thickness (Using method 2) of the ultidirectional Samples Due to 2oisture
-J 0) C a0 e 0
0
a) $4 : .1-,1 O .4.2 . .1method for the measurement of resistance was modified. The modification assumes that the sample surfaces form equipotential sheets; this was proven to be an incorrect assumption. However, within the vicinity of the measurement points, the electical potential between the two surfaces was constant. Therefore, the measurements made using this method are both reliable and accurate. As shown in Figure 13, this procedure also gives the predicted correlation between the normalized change in resistance and the moisture content.
The small number of data points (plotted in Figures 10 through 13) is due to the thick samples' slow rate of moisture absorption; time constraints precluded the achievement of higher moisture concentrations. For more information about moisture absorption in graphite epoxy composites, see Appendix B.
Resistance Change,
R
M
Figure 13. Change in Resistance Across the Thickness (Using Method 3) of the Multidimensional
.8 a,
.6
0 C-) 0 t .4 0 .2I--,
r1 c7 -I! -· 7 - -; L r^ ~ D * .I· nIV. CONCLUSIONS AND RECOMMENDATIONS
An effective method for the determination of moisture content of graphite epoxy composites is to measure the change in electrical resistance. For unidirectional composites, it was found that the normalized change in resistance across the width is proportional to the moisture content squared. For multidirectional composites, it was found that the normalized change in resistance across the thickness is directly proportional to the moisture content. In both cases, it was found that the resistance across the length of the samples was not affected by moisture content.
The presence of contact resistance was found to be minimized by using a modification of the four terminal resistance measurement. However, this method requires much wiring and instrumentation (e.g. 4 probes, volt meter, amp meter, and division of V/I). In order to avoid this, the author recommends that when the piece is produced, two small metal plates (or more than two for averaging over the piece) should be embedded in the two surfaces of the material. These plates should be accessible from the outside, and they should be in direct contact with the graphite fibers. The plates can then be used as electric terminals which would be used for moisture measurements with an ohm meter. Another way would be to embed accessible fine metal meshes at each surface. This would allow the measurement of the average resistance over the piece.
utilized as an inspection technique; it could detect nonuniformities in the material. The resistance across the piece is greatly affected by the number of fibers and by how closely these fibers are packed. These nonuniformities are reflected in the large variations between the samples' resistance measurements.
The author recommends that the experiments described in this thesis be repeated - using the samples embedded with metal terminals or metal mesh. An investigation upon the effect of the volume fraction of fibers on the overall resistance is also recommended. This will aid in the determination of the proportionality constant of the
correlations found in this paper as a function of the fiber volume fraction. It will also help to determine if the above-mentioned method is an effective means of detecting nonuniformities in the graphite epoxy composite. Finally, future tests should determine the effects of stress and temperature upon the resistance. This will permit a more wide-spread application of these procedures.
Appendix A
STATISTICAL SUMMARY OF THE EXPERIMENTAL RESULTS
The following Tables present the average values and the standard deviation of the experimental data.
Table 2
Resistance Measurement Across The Length of The Unidirectional Samples avg. of W (;o)
0.00
.41 .53 .78 .84 1.12 S.D. of AW.
W
0.00 .13 .06 .06 .05 .06 avg of R(A) 3.71 3.67 3.61 3.49 3.55 3.56 S.D. of R .51 .68 .70 .59 .52 .65 Table 3Change in Resistance Across the Width of The Unidirectional Samples
iWv) S.D.Y
W lta) 0.00 .41 .53 .78 .84 0.00 .13 .06 .06 .05 37.3 15.7 /aR.D.s. D. (R
R(l) 29.2 30.4 31.6 33. 5 35.3 S.D. R 11.7 12.9 13.6 13.2 14.6 0.00 .22 .28 .34 .43 0.00 .13 .16 .21 .181 12
.06
.51 .1Table 4
Resistance Measurement (Methode 2) Across The Length of The Multidirectional Samples avg. of a)/) 0.00 .29 .74 .84 S.D. of 4W 0.00 .05 .27 .31 avg of R(%A) S.D. of R .19 .02 .20 .20 .19 .04 .03 .03 Table 5
Change in Resistance (Measurement Methode Thickness of The Multidirectional Samples
W(.)
S.D.
AV
w
w
0.00 .06 .11 .32 0.00 .01 .02 .03 R(~-) 8.05 10.67 11.62 17.38 S.D. R 1.86 2.10 2.02 3.25 1) Across The S D. .%0.00
.08
.14
.21
0.00
.34 .47 1.19 Table 6Change in Resistance (Measurement Methode 2) Across The Thickness of The Multidirectional Samples
0.00 .33 .38
S.D.
W
w
0.00 .01 .01 R(-) 1.15 1.42 1.50 S.D. R .27 .27 .35 AR0.00
.25 .31 S. D. -q0.00
.08 .04 1.62 .3558
.02
.432 .14Table 7
Change in Resistance (Measurement Methode 3) Thickness of The Multidirectional Samples
Wae) s.D.
at
R(4) S.D. R _-0.00 0.00 2.63 .46 0.00 .48 .04 6.15 1.33 1.32 .60 .05 7.98 1.69 2.02 .95 .05 12.19 2.52 3.82 Across The S.D. R0.00
.13 .20 .17Appendix B
MOISTURE ABSORPTION BY COMPOSITES
Moisture absorption of graphite epoxy composites may be modelled using Fick's equation [5] (See Figure 14):
C
D
zc (11)where
c=moisture concentration t=time, seconds
D=moisture diffusion coefficient, mm /sec
Assuming that the moisture diffusion coefficient is only a function of temperature, as well as assuming that the initial conditions and the boundary conditions are (See Figure 14)
c=c. for O<x<h and t<O
c=c, for x=O and x=h and t>O
then, Crank[6] gives the following solution to Fick's equation
CO. C;,_o =
1-- S-2
I .- P / , ) .- ____(h(12
)'where o
c = average moisture concentration in the composite.
Shen and Springer [7] correlate Equation 2 and experimental data. (See Figure 15.)
Co
- c4
-
-- hN%- -70 IN.
x
z
Fi ure 1.
eo
;i . non of -ti.oe ouidiry
on ditirons
s:cd
in the Solution of Fick' s Equation
0.8 -1
I
03 0.6 G4 0.001. Figure 15. CO * .fiha h 0.I t^ aI/h} 4I .- l .0Comparison of Analytical And Measured Moisture Absorption And Desorption Values For Unidirectional And W/4 Graphite Epoxy Composites.
(Taken From Reference 5)
Grophile T- 300
-- Fiberile 1034
(vf 0.65 to068)
o ; / <~~Anlytical
Absorplion and Desorplion
,, ,,, 1111 1 Itll I I I I I I 1 n - . A__ I I .. I ...J UIJ I ... I I I I I I - ----!II i I I OE . i W I [ E I I I J ! I · I I ] I I Z i & ~ M ![ I ~~~j
Tsai and Hahn [41 give an empirical formula for finding D as a function of temperature for graphite epoxy composites.
D=6.51 exp(-5722/T) (13)
where
T=absolute temperature, OK
They [4] also give a formula for estimating the equilibrium moisture concentration for graphite epoxy composites.
C
0
.0/8 (14)where
0=relative humidity, %
By using Equations 2 and 3, it is possible to determine the time required for a sample to reach a given fraction of equilibrium moisture concentration. For example, for a sample 0.25 inches thick, the time t /2 for which (Z-cO)/(c.-c )=l/2 at a temperature T=373°K (100°C) is
t /2 =16 days. (15)
And for the same conditions, t /=39 days and t q4 0=70 days.
This gives an estimate of the time required to perform the experiments described in this thesis.
REFERENCES
1. Shen, C.H. and Springer, G.S., "Effects of Moisture and Temperature on the Tensile Strength of Composite Materials," Journal of Composite Materials, Vol. 11, 1977, pp. 2-16
2. Belani, J.G. and Broutman, L.J., "Moisture Induced Resistivity Changes in Graphite - Reinforced Plastics," Composites, Vol. 9, N. 4, October 1978 3. Holm, Ragnar, Electric Contacts Theory and Application,
Fourth Edition, Springer - Verlag New York Inc., New York, 1967
4. Tsai, S.W. and Hahn, H.T., Introduction To Composite
Materials,
Technomic Publishing
Co.,
Inc.,
Westport, Connecticut, 1980
5. Springer, G.S., "Environmental Effects on Epoxy Matrix Composites," Composite Materials: Testing and Design (Fifth Conference), ASTM STP 674, 1979, pp. 291-312
6. Crank, J., The Mathematics of Diffusion, Second Edition,
Clarendon
Press,
Oxford, 1975
7. Shen, C.H. and Springer, G.S., "Moisture Absorption and Desorption of Composite Materials," Journal of