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ASTM Selected Technical Papers
Fiber-Strengthened Metallic Composites
By
Aerospace Panel of the ASTM-ASME Joint Committee on Effect of Temperature on the Properties of Metals
Aerospace Panel of the ASTM-ASME Joint Committee on Effect of Temperature on the Properties of Metals
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ISBN-10:
0-8031-6179-4
ISBN:
978-0-8031-6179-5
No. of Pages:
185
Publisher:
ASTM International
Publication date:
1967

An analysis of the creep deformation of fiber reinforced metallic composites was developed. Equations for predicting the creep rate and stress-rupture properties of fiber reinforced metallic composites were presented. Stress-rupture and creep tests were conducted at 1200 and 1500 F on tungsten fiber reinforced copper composites. The results of these tests were used to verify the validity of the equations developed in the analysis. A discussion was presented relating the results obtained with the model system to more practical fiber reinforced composite systems for stress-rupture applications. The stress-rupture strengths obtained with the tungsten-copper model system compared favorably with those of existing superalloys and demonstrated the potential of fiber reinforced metallic composites in stress-rupture applications at elevated temperatures.

1.
Jech
,
R. W.
,
McDanels
,
D. L.
, and
Weeton
,
J. W.
, “
Fiber Reinforced Metallic Composites
,”
Proceedings of the Sixth Sagamore Ordnance Materials Research Conference
, Report No. MET661-601,
Syracuse University Research Institute
,
1959
, pp. 116–143.
McDanels
,
D. L.
,
Jech
,
R. W.
, and
Weeton
,
J. W.
, “
Metals Reinforced with Fibers
,”
Metals Progress
, Vol.
78
, No.
6
,
12
1960
, pp. 118–121.
2.
McDanels
,
D. L.
,
Jech
,
R. W.
, and
Weeton
,
J. W.
, “
Stress-Strain Behavior of Tungsten-Fiber-Reinforced Copper Composites
,” NASA TN D-1881,
National Aeronautics and Space Administration
,
1963
.
McDanels
,
D. L.
,
Jech
,
R. W.
, and
Weeton
,
J. W.
, “
Analysis of Stress-Strain Behavior of Tungsten-Fiber-Reinforced Copper Composites
,”
Transactions, American Institute of Metallurgical Engineers
 0096-4778, Vol.
233
, No.
4
,
04
1965
, pp. 636–648.
3.
McDanels
,
D. L.
, “
Electrical Resistivity and Conductivity of Tungsten-Fiber-Reinforced Copper Composites
,” NASA TN D-3590,
National Aeronautics and Space Administration
,
1966
.
4.
Sutton
,
W. H.
, “
Development of Composite Structural Materials for Space Vehicle Applications
,”
Journal, American Rocket Society
 0095-9073, Vol.
32
, No.
4
,
04
1962
, pp. 593–600.
5.
Cratchley
,
D.
, and
Baker
,
A. A.
, “
The Tensile Strength of a Silica Fibre Reinforced Aluminum Alloy
,”
Metallurgia
, Vol,
69
, No.
414
,
04
1964
, pp. 153–159.
6.
Kelly
,
A.
, and
Tyson
,
W. R.
, “
Fibre-Strengthened Materials
,”
High-Strength Materials
,
Zackay
V. F.
, ed.,
Wiley
,
New York
,
1965
, pp. 578–602.
7.
Petrasek
,
D. W.
, “
Elevated-Temperature Tensile Properties of Alloyed Tungsten Fiber Composites
,” NASA TN D-3073,
National Aeronautics and Space Administration
,
1965
.
Petrasek
,
D. W.
Elevated-Temperature Tensile Properties of Tungsten Fiber Composites
,”
Transactions, American Institute of Metallurgical Engineers
 0096-4778, Vol.
236
, No.
6
,
06
1966
, pp. 887–896.
8.
Jech
,
R. W.
,
Weber
,
E. P.
, and
Schwope
,
A. D.
, “
Fiber-Reinforced Titanium Alloys
,” Reactive Metals, Vol.
2
,
Clough
W. R.
, ed.,
Interscience
,
New York
,
1959
, pp. 109–116.
9.
Dean
,
A. V.
, “
The Reinforcement of Nickel-Base Superalloys with High Strength Tungsten Wires
,” NGTE-R-266,
National Gas Turbine Establishment
,
England
,
1965
.
10.
Ellison
,
E. G.
, and
Harris
,
B.
, “
The Elevated Temperature Properties of a Nickel Alloy Reinforced with Tungsten Wires
,”
Applied Materials Research
 0570-4847, Vol.
5
, No.
1
,
01
1966
, pp. 33–40.
11.
Carlson
,
R. G.
, “
Aluminum-Boron Composites for Potential Jet Engine Compressor Blade Application
,” Report No. DM 65-441,
General Electric Co.
,
1965
.
12.
Petrasek
,
D. W.
, and
Weeton
,
J. W.
, “
Alloying Effects on Tungsten-Fiber-Reinforced Copper-Alloy or High-Temperature-Alloy Matrix Composites
,” NASA TN D-1568,
National Aeronautics and Space Administration
,
1963
.
Petrasek
,
D. W.
, and
Weeton
,
J. W.
, “
Effects of Alloying on Room-Temperature Tensile Properties of Tungsten-Fiber-Reinforced Copper-Alloy Composites
,”
Transactions, American Institute of Metallurgical Engineers
 0096-4778, Vol.
230
, No.
5
,
08
1964
, pp. 977–990.
13.
McDanels
,
D. L.
, and
Signorelli
,
R. A.
, “
Stress-Rupture Properties of Tungsten Wire from 1200 to 2500 F
,” NASA TN D-3467,
National Aeronautics and Space Administration
,
1966
.
14.
McDanels
,
D. L.
,
Signorelli
,
R. A.
, and
Weeton
,
J. W.
, “
Analysis of Stress-Rupture Properties of Tungsten-Fiber-Reinforced Copper Composites
,” proposed NASA Technical Note,
National Aeronautics and Space Administration
.
15.
Jech
,
R. W.
,
Springborn
,
R. H.
, and
McDanels
,
D. L.
, “
Apparatus for Stress-Rupture Testing of Filaments in a Controlled Atmosphere
,”
Reviews of Scientific Instruments
 0034-6748, Vol.
35
, No.
3
,
03
1964
, pp. 314, 315.
16.
Signorelli
,
R. A.
,
Petrasek
,
D. W.
, and
Weeton
,
J. W.
, “
Interfacial Reactions in Metal-Metal and Ceramic-Metal Fiber Composites
,”
Modern Composite Materials
,
Krock
Richard
and
Broutman
Lawrence
, eds.,
Addison-Wesley
,
Reading, Mass.
,
1967
.
17.
Preston
,
O.
, and
Grant
,
N. J.
, “
Dispersion Strengthening of Copper by Internal Oxidation
,”
Transactions, American Institute Metallurgical Engineers
 0096-4778, Vol
221
, No.
1
,
02
1961
, pp. 164–173.
18.
Lund
,
C. H.
, “
The Use of Nickel-Base Alloys in the Rotating. Parts of Gas Turbines for Aerospace Applications
,” DMIC Memo 145,
Battelle Memorial Institute
,
1962
.
19.
VanEcho
,
J. A.
, and
Simmons
,
W. F.
, “
Mechanical and Physical Properties of Three Superalloys-MAR-M200 and MAR-M322
,” DMIC Memo 193,
Battelle Memorial Institute
,
1964
.
20.
Campbell
,
J. E.
, “
Compilation of Tensile Properties of High-Strength Alloys
,” DMIC Memo 150,
Battelle Memorial Institute
,
1962
.
21.
Arridge
,
R. G. C.
,
Baker
,
A. A.
, and
Cratchley
,
D.
, “
Metal Coated Fibres and Fibre Reinforced Metals
,”
Journal of Scientific Instruments
 0950-7671, Vol.
41
, No.
5
,
05
1964
, pp. 259–261.
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