MIL-HDBK-17-4 - Composite Materials Handbook Vol4 [US DOD 1999] 4AH Episode 10 ppt

... (m/m/°C, in./in./°F) MIL- HDBK- 17- 4 Volume 4 of 4 21 September 1999 DEPARTMENT OF DEFENSE HANDBOOK COMPOSITE MATERIALS HANDBOOK VOLUME 4. METAL MATRIX COMPOSITES This handbook is for guidance ... fusion processes. MIL- HDBK- 17- 4 7 Further discussions of these and other issues are provided in Section 2. Specific uses of handbook data are beyond the scope and...

Ngày tải lên: 27/06/2014, 18:20

... 75 8.3x10-5 12. 1 - - 112 122 22.1 39.5 HIP Sheet 5 ksi Helium - 16 212_ C B934027 75 8.3x10-5 12 - - 116 125 16.8 22 HIP Sheet 5 ksi Hydrogen - 16213_D B934027 75 8.3x10-5 12. 5 - - 114 125 17.2 27.1 ... 75 2x10-3 13 111 117 124 127 20.2 - HIP Foil air - 16211_B B934027 75 8.3x10-5 12. 4 - - 114 124 20.7 37.8 HIP Sheet 5 ksi Helium - 16210_A B934027 75 8.3x10-5 11.9 - - 110 120 2...

Ngày tải lên: 10/08/2014, 11:21

... SECTION 11 1 3 .1. 3 DATA PRESENTATION FORMAT AND ORGANIZATION 11 1 3 .1. 3 .1 Manuals 11 1 3 .1. 3.2 Electronic 11 1 3.2 REINFORCEMENT PROPERTIES 11 1 3.2 .1 INTRODUCTION 11 1 3.2.2 ALUMINA FIBERS 11 1 3.2.3 ... FIBERS 11 1 3.2.9 OTHER FIBERS 11 1 3.2 .10 OTHER REINFORCEMENTS 11 1 3.3 PROPERTIES OF MATRIX MATERIALS 11 1 3.3 .1 INTRODUCTION 11 1 3.3.2 ALUMINUMS 11 2 3.3.3 CO...

Ngày tải lên: 10/08/2014, 11:21

... (thermochemical)/in. 2 -s watt/meter 2 (W/m 2 ) 1.634 24 6 E+06 Btu-in/(s-ft 2 -°F) W/(m K) 5.1 92 204 E+ 02 Btu/lb F Joule/gram-Kelvin 4.1868** (or Btu#lb. -1 #F -1 )(J/g#K) or J#g -1 #K -1 ) Btu/[(hr)(ft 2 )(F)/ft] ... 3.048 000 E-01 ft 2 m 2 9 .29 0 304 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...

Ngày tải lên: 10/08/2014, 11:21

... MIL-HDBK-17-4 57 1.2 .3. 3.4 Magnesium This section is reserved for future use. 1.2 .3. 3.5 Nickel This section is reserved for future use. 1.2 .3. 3.6 Titanium Titanium matrix composites have been ... condition of 73 5°F ( 23 3 C) at ambient laboratory relative humidity; 2) a material condition where, immediately following consolidation/cure, the material is stored at 73 5°F ( 23 3 C)...

Ngày tải lên: 10/08/2014, 11:21

... 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,...

Ngày tải lên: 10/08/2014, 11:21

... condition Tensile 5 3 15 Fatigue 5 3 15 Creep 5 3 15 Crack Growth 5 3 15 Hardness 5 3 15 Microstructure (with magnification) 5 3 15 Chemical Analysis 5 3 15 Coefficient of Thermal Expansion 5 3 15 Density 5 ... Thermal Expansion (a) 5 1 15 min. per dir. Specific Heat (b) 5 1 5 Thermal Conductivity (a) 5 1 15 Electrical Conductivity (a) 5 1 15 Density (c)...

Ngày tải lên: 10/08/2014, 11:21

... Metal Matrix Composites,” Annual Book of ASTM Standards, Vol 15.03, American Society for Testing and Materials, West Conshohocken, PA, 19 97, pp. 173 - 177 . 1.4.2.2 ASTM Standard D3410- 87, "Standard ... to be located along a constant ge- MIL-HDBK- 17- 4 94 MIL-HDBK -73 1 Thermography MIL-HDBK -73 2 Acoustic Emission MIL-HDBK -73 3 Radiography MIL-HDBK -78 7 Ultrasonic These documents...

Ngày tải lên: 10/08/2014, 11:21

... Metall. Mater., Vol 28, 1993, pp. 1 583 -1 588 . 1.4.2.13.14(f) Galbraith, J.M., Rhyne, E.P., Koss, D.A., and Hellmann, J.R., “The Interfacial Failure Sequence during Fiber Pushout in Metal Matrix Composites,” ... MIL-HDBK-17-4 103 1 .8 FIBER COATINGS, INTERFACES AND INTERPHASES TESTING AND ANALYTICAL METHODS 1 .8. 1 INTRODUCTION 1 .8. 2 MECHANICAL PROPERTY TEST METHODS 1 .8. 3 PHYSIC...

Ngày tải lên: 10/08/2014, 11:21

... matrix manufacture Date of data submittal 6 /98 Date of testing 5 /96 -7 /97 Date of analysis 8 /98 MATRIX PROPERTY SUMMARY Temperature 75°F 400°F 600°F 800°F 90 0°F 1000°F Environment Air (1) Air Air ... (2) F tu Distribution ANOVA (ksi) C 1 2. 89 C 2 12 .9 No. Specimens 7 No. Lots 2 Approval Class Screening Mean 12.4 12.3 11.4 Minimum 11 .9 12.0 Maximum 13.0 12.6 E t C.V.(%) 3. 39 (M...

Ngày tải lên: 10/08/2014, 11:21

... A1(a) The effect of specimen thickness on the observed debond strength of SCS-6/Ti24 -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], ... OTHER/TITANIUM 3.9 OTHER MATRIX COMPOSITES MIL-HDBK-17-4 APPENDIX A 152 A1. FIBER PUSHOUT TABLE A1(a) Debond load vs. specimen thickness for SCS-6/Ti-24 -11 (Section 1.4.2....

Ngày tải lên: 10/08/2014, 11:22

... applica- bility of this method for various composite systems. However, Tables A1(a) and A1(b) in Appendix A pro- vide some useful information on the SCS -6/ Ti-24-11 composite system, in addition to giving ... is to test thicker materials which can withstand compressive loads. This may not be an option due to the high cost of thick materials or difficulties in manufacturing thick comp...

Ngày tải lên: 12/08/2014, 03:20

... Air Air Air Air Air Air Fiber Volume (%) 152535353541 Strain Rate (1/s) 1 10 -3 1 10 -3 1 10 - 5 1 10 - 4 1 10 - 3 1 10 -3 Mean 24 17 91 Minimum 31 Maximum 151 C.V.(%) B-value F pl 1 Distribution (ksi) ... Air Air Air Air Air Air Fiber Volume (%) 152535353541 Strain Rate (1/s) 1 10 -3 1 10 - 3 1 10 - 5 1 10 -4 1 10 - 3 1 10 -3 Mean 137 195 198 200 226 248 Minimum 136 192 201 245 M...

Ngày tải lên: 12/08/2014, 03:20

... of interfacial failure pos- sible. MIL-HDBK-1 7-4 76 FIGURE 1.4.2.13.5(b) Tabletop fiber pushout testing system used at NASA Lewis Research Center. MIL-HDBK-1 7-4 66 ments. A sudden divergence ... complete removal of the fiber. MIL-HDBK-1 7-4 69 FIGURE 1.4.2.5(a) Middle tension specimen, M (T). FIGURE 1.4.2.5(b) Single-edge tension specimen, SE (T). MIL-HDBK-1 7-4...

Ngày tải lên: 13/08/2014, 17:20

... 25 35 41 [0] Tension, 1-axis SS-SSSS SSSSSS- SS-SSS- SSSS-S- SSSS-S- SS-SSS- SSSS [90] Tension, 2-axis SS-SSSS SSSSSSS SS-S SS-SSSS Classes of data: F - Fully approved, S - Screening in order: ... Strength/Modulus/Poisson’s Ratio/Strain-to-failure/Proportional Limit/0.02-offset-strength/0.2-offset-strength. * Raw data tables in Appendix C. MIL-HDBK-1 7-4 133 MATERIAL: SCS-6/Ti-...

Ngày tải lên: 13/08/2014, 17:20