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,...

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... 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...

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... 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...

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... 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...

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... 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...

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... 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...

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... 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...

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... 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...

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... 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...

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... 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],...

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