Composite Materials Handbook Part 7 pot

... 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

... . . . . . . . . . . . . 4- 11 4- 11 4- 11 4- 12 4- 13 4- 15 4- 16 4- 17 4- 17 4- 19 4- 19 4- 20 4- 21 4- 21 4- 22 4- 22 4- 24 4- 24 4- 24 4- 24 4- 24 4-25 xviii CONTENTS SECTION 1 -WELDING MATERIALS. . . . . . . ... . . . . . . . . . . . . . . . . . . . . . . . . . Page 4- 1 4- 1 4- 2 4- 2 4- 3 4- 3 4- 4 4- 4 4- 5 4- 5 4- 7 4- 9 4- 9 4- 9 4- 9 4- 9 4-...

Ngày tải lên: 11/08/2014, 18:20

... be in the above ranges.) USES: This wire is recommended for welding 50 56 ,50 83, 50 86 ,51 54, and 53 56 aluminum alloys. USE THIS WIRE FOR WELDING ALUMINUM LANDING MATS. PROCEDURES: Wire and joint to ... POSITIONS Material Thickness (in.) .037 . 050 .062 .1 25 .187 Travel Amps volts Speed (ipm) 70 17 20-40 85 18 20 -50 100 18 25- 35 150 20 15- 25 150 20 10-20 (NOTE: The abov...

Ngày tải lên: 11/08/2014, 18:20

... Base Alloy (A) in ratios: By Volume -1 part A to 1 part R By Weight -2 parts A to 1 part R 3) Working time after mixing is approximately 2 to 5 minutes at 70 °0F. 4) Deposits reach handling strength ... information. 2) Mix reactor (R) into Base Alloy (A) in ratios: By Volume -2 parts A to 1 part R By Weight -4 parts A to 1 part R 3) Working time is approximately 30 minutes at room...

Ngày tải lên: 11/08/2014, 18:20

... 7. 2. Essentials of transistor action. 228 The Coming of Materials Science as a moving testimony to the brilliance of his theoretical and experimental investigations”. The essence of ... hardness in terms of the area of the indentation projected in the plane of the tested surface. Meyer’s empirical law then stated that if W is the load and d the...

Ngày tải lên: 11/08/2014, 20:21