impact energy of aisi 3o2 stainless steel - Digital Collections

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$Standard X-ray Diffraction Powder Patterns$

$Standard X-ray Diffraction Powder Patterns$

$Standard X-ray Diffraction$

Superalloys (Alloys <strong>of</strong> Co, Ni, Cr, W, Mo) TENSILE ————— YIELD 148 A-286 [3j, HT. TR* CO IOO 8O 6O HEAT TREATMENTS 1. I8OO°F,WQ a AGED 16 HRS. AT 1325 °F, AC 2. I9OO°F, WQ a AGED 16 HRS AT I3OO°F, AC 3. I85O°F, OQ + 4 HRS. AT I55O°F, AC a AGED 16 HRS. AT I30O°F, A.C. O 5O IOO ISO ZOO 25O TEMPERATURE, °K STRENGTH OF SUPERALLOYS 3OO IOO ISO 2OO 25O 3OO TEMPERATURE, °K ELONGATION OF SUPERALLOYS
80 CHARPY V CHAPPY U 149 7O MULTIMET { N - 155) , CONDITION*! [67] A - 286 [3] — CONDITION*2 6O 50 HAYNES ALLOY No. 25 ( L~6O5) CONDITION*! [67] -O J. 4O 3O I9-9DL [97] CONDITION* 3' I9-9DL [97] ( CONDITION 2O 19 -9DL [97],- CONDITION*5' 10 SAMPLE CONDITION 1. HOT ROLLED a STRESS RELIEVED AT 22OO °F. 2. I8OO°F, WQ a AGED 16 HRS. AT 1325 °F, A.C. __ 3. ANNEALED AT I8OO°F, A.C. 4. WARM WORKED a STRESS RELIEVED AT I2OO °F 5. COLD DRAWN a STRESS RELIEVED. I 5O IOO ISO 200 250 3OO TEMPERATURE, °K IMPACT ENERGY OF SOME SUPERALLOYS
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! -H -i ; \3 UNIVERSITY Oh ARIZONA
Page 6 and 7:
Foreword The advent of space vehicl
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perform an evaluation of data which
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straight lines, and intermediate or
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compromise between simplicity and u
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NOIJLVnidlAlOO SIH-L Nl SHdVdO NO N
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50 IOO ISO 2OO 25O 3OO TEMPERATURE,
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9OxlO 3 SO 70 ROLLED, FORGED, EXTRU
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eoxio3 7O 6O 22I8-T6I OJ 2OI8-T6l[4
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5O 8 4O o> o Qi Q. 20 IO T4 [4, 64,
Page 24 and 25:
TO x icr 10 6O 50 LU 4O 30 / HI8 [4
Page 26 and 27:
8Ox IO F, AS ROLLED (PLATE) [4] TEN
Page 28 and 29:
7O x IQ IOO ISO 2OO TEMPERATURE, °
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, AS ROLLED (PLATE) IOO ISO 2OO 25O
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8Ox IO TENSILE — — — YIELD iO
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5O IOO I5O ZOO 25O 3OO TEMPERATURE,
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5O IOO I5O 2OO 25O 3OO TEMPERATURE
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9O x IO IOO ISO 2OO 25O 3OO TEMPERA
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5O IOO ISO 2OO 250 3OO TEMPERATURE,
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55 28 5O 45 4O 35 o> o 3O 25 20 T6l
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7OxlO 3O 6O T6,FORGED[4] 5O CḺ 40
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40 35 3O Q 25 c 2O •4- C ** I 5 \
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7O x IO 34 TENSILE — YIELD IOO IS
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Copper and Its Alloys so x ic 7O 6O
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30O xl 28O 26O CONDITION A AT »/2H
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I6O x IO* ISO 4O -A Be-Zn, i-HT[80]
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42________ j | 67-33, 4O% C.D. [l (
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B ALLOY _____44 COMPOSITIONS FREE C
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150 I4O 46 X IW I l < ' NOMINAL COM
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x icr ISO I4O I3O 48 COMPOSITIONS C
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50 D 3 ISO x l( COMPOSITIONS COMPLY
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I3U X 1 I4O 130 I2O u 52 COMPOSITIO
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ieox icr I7O I6O ISO \ 54 COMPOSITI
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i4o x icr 56 I3O 120 MO IOO ASTM TY
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ISO x IO I4O ___________58_________
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I4O I3O icr 6O NOMINAL COMPOSITIONS
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Nickel and Its Nonferrous Alloys !5
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3OO 28O CHAPPY V ———— I20D
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co 6O 50 o -- 4O CJ •E 3O 66 HOT
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70 60 68_______ I i ANNEALED [17,33
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8O 7O ___________TO__________ TREAT
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Titanium and Its Alloys 72 ISOxlO*
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280 x 10 27O 260 15 Cr, AS FORGED [
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28O x IO 27O 26O ANNEALED, (.24% CA
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28O x IO 27O 26O HEAT TREATED 1725
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4O SO 35 CO 01 30 25 OJ TA54, AS EX
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AS EXTRUDED [25,81,103] HOT ROLLED,
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soxic 8O 7O 6O tO Q. ~ 50 CO CO rr
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4O 86 35 3O CO o> 25 CM 2O a* u \_
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4O 88 35 to HK 31 A-H24 [25] 10 25
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90 7Ox 5O IOO ISO 2OO 25O 3OO TEMPE
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6O xlO 50 92 _____ ALL SPECIMENS AN
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34OxlO 32O 3OI-N COLD ROLLED 65%, (
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COLD DRAWN,(7I %R.A.)[63] ^COLD DRA
Page 112 and 113: 98 28O x IO3 ANNEALED [4l] 10% COLD
Page 114 and 115: IOO COLD DRAWN,(TO U.T.S. 2IO,OOO p
Page 116 and 117: 28OxlO3 24O IO2 15 % COLD DRAWN [r
Page 118 and 119: 104 ANNEALED [7l], (I INCH GAGE LEN
Page 120 and 121: IOO IO6 vt o» o 8O ANNEALED [2,4l,
Page 122 and 123: IO8 ANNEALED [41,71] IOO ISO ZOO TE
Page 124 and 125: 80 no 70 to Of 6O COLD DRAWN IO % [
Page 126 and 127: x» IOO 9O 8O «!. 70 H- •* e> 60
Page 128 and 129: 114 JQ i ————ANNEALED H—
Page 130 and 131: 5O CHAPPY K REF [50] 116 50 IOO ISO
Page 132 and 133: 80 7O CHAPPY K PER [50] 118 60 5O A
Page 134 and 135: Ferritic and Hardenable Stainless S
Page 136 and 137: 122 28OxlO3 26O 24O QUENCHED AND TE
Page 138 and 139: 124 I3O 120 c/ C/5 UJ or no 100 9O
Page 140 and 141: 28OxlO 126 AMS-5643B,(I7-4PH), COND
Page 142 and 143: Low Alloy Constructional Steels iou
Page 144 and 145: e.\j\j x I9O ISO I7O I6O ISO ._ I4O
Page 146 and 147: 7O _____________132 i I I COMPOSITI
Page 148 and 149: 25 134 O CM 2O — 10 OL —^ 30ON
Page 150 and 151: NOMINAL COMPOSITION 9% Ni - .11% C
Page 152 and 153: 7O 65 6O 55 5O 45 4O __^_____ 138 Q
Page 154 and 155: 38O x iO ; 34O I4O OQ 8 TEMPERED 4
Page 156 and 157: I2O IOO OQ a TEMPERED I HR. AS SHOW
Page 158 and 159: 22O x IO3 144 ZOO OQ a TEMPERED AT
Page 160 and 161: 3O 25 _______________146 OQ a TEMPE
Page 164 and 165: 1 ———————————
Page 166 and 167: 152 I9O x IO 3 180 I7O I6O 150 I4O
Page 168 and 169: Brazing and Soldering Metals 3OxlO
Page 170 and 171: 12 x IO 156 1.6 Ag - 15 Sn - 83.4 P
Page 172 and 173: 158 I4O x IO 5OCu -5OZn 93O°F ANNE
Page 174 and 175: Miscellaneous Alloys and Pure Metal
Page 176 and 177: 20O x IO" 162 "Si 180 a. c/fieo UJ
Page 178 and 179: 120 no ______________164 SPECIMENS
Page 180 and 181: 60 166 to 50 "5 4O c 3O HOT ROLLED
Page 182 and 183: 24OxlO3 ____________168__________ H
Page 184 and 185: 3OO x ICf I7O 28O 26O 24O ALLOY A,
Page 186 and 187: isoxicr u 172 I4O I2O £100 o en 80
Page 188 and 189: 5O 174 40 HIGH PURITY — VACUUM AR
Page 190 and 191: 176 POLYTETRAFLUOROETHYLENE ——
Page 192 and 193: 29. A. S. Eldin and S, C. Collins,
Page 194: 84. E. EL Schmidt, Low temperature
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