Composite Materials Handbook Part 4 docx
Composite Materials Handbook Part 4 docx
... Joining Techniques for Metal
Matrix Composites,” Boeing Co., Report: AMMRC TR- 84- 35, August 19 84.
1.2.8 .4. 3 .4( a) Nedervelt, P. D., and Burns R. A., “Metal Matrix Composites Joining and Assembly
Technology,” ... Report No. WL-TR-93 -40 83, September 1993.
1.2.8 .4. 3 .4( b) Lienert, T., Lane, C., and Gould, J., “Selection and Weldability of Al. Metal Matrix
Composites,” ASM Handbook,...
Composite Materials Handbook Part 8 docx
... 4,
pp. 543 - 549 .
1 .4. 2.13. 14( g) Chandra, N., and Ananth, C.R., “Analysis of Interfacial Behavior in MMCs and IMCs by
the Use of Thin-Slice Push-Out Tests,” Composites Sci. Technol., Vol 54, 1995, ... High-Temperature Structural Materials, R.A. Lowden et al., Eds., Mater. Res.
Soc. Proc., Vol 365, 1995, pp. 353-3 64.
1 .4. 2. 14 ASTM Standard E3 84, “Standard Test Method for Microha...
Composite Materials Handbook Part 12 pps
... 1 14 145 1.11 - Ti-weave
+/- 30 24 87H 149 75 1x10 -4 22 67 75 112 144 >1.5 - Ti-weave (2)
+/- 30 23 87H 149 75 1x10 -4 24 48 71 115 145 0.99 - Ti-weave
+/- 30 22 87H 149 75 1x10 -4 20 65 97 146 147 ... 1x10 -4 23 44 60 105 - - - Mo-weave (1)
+/- 30 H16 D890053 75 1x10 -4 23 48 60 108 179 1.66 - Mo-weave
+/- 30 26 87H 149 75 1x10 -4 24 58 74 1 14 148 1. 14 - Ti-weave
+/- 30...
Composite Materials Handbook Part 1 pot
... Tension 65
1 .4. 2.2 Compression 65
1 .4. 2.3 Shear (in-plane) 66
1 .4. 2 .4 Fatigue 66
1 .4. 2 .4. 1 Scope 66
1 .4. 2 .4. 2 Specimen design 66
1 .4. 2 .4. 3 Waveforms 66
1 .4. 2 .4. 4 Control mode 67
1 .4. 2 .4. 5 Compressive ... 89
1 .4. 3.9 Stress corrosion cracking 89
1 .4. 3.10 Wear 89
1 .4. 3.11 Impact 89
1 .4. 3.12 Damping 89
1 .4. 4 PHYSICAL PROPERTY TEST METHODS 89
1 .4. 4.1 Density...
Composite Materials Handbook Part 2 pot
... kelvin (K) T = (T + 45 9.67)/1.8
foot meter (m) 3. 048 000 E-01
ft
2
m
2
9.290 3 04 E-02
foot/second meter/second (m/s) 3. 048 000 E-01
ft/s
2
m/s
2
3. 048 000 E-01
inch meter (m) 2. 540 000 E-02
in.
2
meter
2
... (N) 4. 448 222 E+03
ksi (kip/in.
2
) MPa 6.8 94 757 E+00
ksi√in. megapascal √meter 1.0989
(MPa#m 1/2)***
lbf-in. N-m 1.129 848 E-01
lbf-ft N-m 1.355 818 E+00
lbf/in.
2
(psi) p...
Composite Materials Handbook Part 3 pptx
... use.
MIL-HDBK-17 -4
52
REFERENCES
1.1.6(a) Military Standardization Handbook, Metallic Materials and Elements for Aerospace Vehicle
Structures, MIL-HDBK-5F, 1 November 1990.
1.1.6(b) DoD/NASA Advanced Composites ... Vol. 14. 01,
American Society for Testing and Materials, West Conshohocken, PA, 19 84.
(canceled April 28, 1997; now sold in book form called “Metric 97”).
1.1.6.3(b) Engine...
Composite Materials Handbook Part 5 pdf
... monotapes
1.3.3.5 .4
Specialized forms
1.3.3.6
Composite materials
1.3 .4
CONTINUOUS FIBER REINFORCED MMC CONSTITUENT MATERIAL PROPERTIES
1.3 .4. 1
Screening
1.3 .4. 2
Acceptance testing of composite materials
This ... Documentation Requirements
MIL-HDBK-17 -4
76
FIGURE 1.3.2 .4( c)
Flat dogbone specimen.
MIL-HDBK-17 -4
60
1.3 .4. 2.1
Composite static properties tests
T...
Composite Materials Handbook Part 7 pot
...
Fatigue
1 .4. 3.6
Fatigue crack growth
1 .4. 3.7
Creep/stress rupture
1 .4. 3.8
Corrosion fatigue
1 .4. 3.9
Stress corrosion cracking
1 .4. 3.10
Wear
1 .4. 3.11
Impact
1 .4. 3.12
Damping
1 .4. 4
PHYSICAL ...
Impact
1 .4. 2. 24
Damping
1 .4. 3
DISCONTINUOUS REINFORCED MMC MECHANICAL PROPERTY TEST METHODS
1 .4. 3.1
Tension
1 .4. 3.2
Compression
1 .4. 3.3
Shear (in-pl...
Composite Materials Handbook Part 9 pptx
... 8.3
x
10
-
5
, 1
x
10
-
4
, 2
x
10
-
3
.
MIL-HDBK-17 -4
125
0
20
40
60
80
100
120
140
0 0.01 0.02 0.03 0. 04 0.05 0.06 0.07 0.08
Stress (ksi)
Strain
1000
o
F
900
o
F
800
o
F
600
o
F
40 0
o
F
75
o
F
FIGURE ... temperatures: 40 0°F (2 04 C)
(Figure 3.3.5.1(f)), 800°F (42 7°C) (Figure 3.3.5.1(g)), and 1000°F (538°C) (Figure 3.3.5.1(h)). At 40 0°F
(2 04 C) there is minimal strai...
Composite Materials Handbook Part 11 ppt
... SCS-6/Ti- 24- 11 (Section 1 .4. 2.13.1).
Specimen thickness
(mm)
Debond load
(N)
. 149 4. 56
.211 6.06
.312 15.6
.322 14. 3
. 343 15.8
.382 19.6
.41 4 18.8
.45 2 21.8
.48 3 26.8
.5 34 31.8
.569 45 .3
TABLE ... the observed debond strength of
SCS-6/Ti 24- 11 composite system (Section 1 .4. 2.13.11).
MIL-HDBK-17 -4
146
0
20
40
60
80
100
120
140
160
10 15 20 25 30 35 40 45
[0],...