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NITRONIC 32

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Journal Articles
Alloy Digest (2018) 67 (9): SS-1294.
Published: 01 September 2018
... Electralloy Nitronic 32 was created to match AISI Type 304 Stainless Steel in corrosion with twice the yield strength. This datasheet provides information on composition, physical properties, and tensile properties. It also includes information on corrosion resistance as well as joining. Filing...
Journal Articles
Alloy Digest (1975) 24 (11): SS-320.
Published: 01 November 1975
... NITRONIC 32 is basically a low-nickel chromium-manganese austenitic stainless steel strengthened by an addition of nitrogen. It has annealed strength approximately two times that of AISI Type 304 stainless steel and comparable corrosion resistance. It is used in such applications as fasteners...
Journal Articles
Alloy Digest (2009) 58 (2): SS-1029.
Published: 01 February 2009
... www.asminternational.org CARLSON ALLOY NITRONIC 60® DOI: 10.31399/asm.ad.ss1029 Table 1 Galling resistance (unlubricated galling resistance of stainless steels) Threshold galling stress(a), MPa (ksi) Condition, nominal hardness, HB 410 416 430 440C 303 304 316 17-4 NTRC 32 NTRC 60 H&SR (352), 410 21 (3) 28 (4) 21 (3) 21...
Journal Articles
Alloy Digest (2018) 67 (10): SS-1295.
Published: 01 October 2018
... :: Fax 440.338.4634 :: www.asminternational.org :: MemberServiceCenter@asminternational.org Published by ASM International® :: Data shown are typical, not to be used for specification or final design. Specific heat, 0 100 °C (32 212 °F), J/kg·K (Btu/ lb·°F) 502 (0.12) Electrical resistivity, m...
Journal Articles
Alloy Digest (1990) 39 (4): SS-304.
Published: 01 April 1990
... 98 (676) 1000 (538) 89 (614) 1350 cm) 68 wm 1500 (816) 50 045) l-l l/2 bar 75 (24 117 (807) ammled205m 600 (316) 92 (634) loo0 (538) 84 (579) 1350 (732) 66 (455) lSO0 (816) 52 (359) l AverageoftriplicatetfmmeacbofUazebeats. 54 i372j 37.5 48 031) 36.5 42 (290) 425 32 (221) 59.5 60 (414) 4s 35 (241...
Journal Articles
Alloy Digest (1990) 39 (8): SS-327.
Published: 01 August 1990
... 1OOhr ill1OOOhrs. F NITRON-IC 40 Type 3475; 19-9DL* NlTRONK40 Type347* 19-9DL* 1200 32 27-32 28-30 21.5 17-26 25 1500 6.4 4-8 5-9 2.8 4.5 4 *ASTM Special Technical Publication No. 160 **ASTM Special Technical Publication No. 124 Copyright © ASM International® 1996 DOI: 10.31399/asm.ad.ss0327 Table 4...
Journal Articles
Alloy Digest (1981) 30 (2): SS-381.
Published: 01 February 1981
...) Tcnsilc Yield Strength Elongation Reduction Tcmpcraturc Strength (0.2% Offset) (2 in. or 50.8mm) of Arca or: (OC) psi tMPa) psi ( MPa) :i : i 75(24) 142000(979) 84000(579) 29 37 lOOO(538) 96000(662) 42000(290) 34 40 1200(649) 84000(5 79) 39000(269) 30 32 1400(760) 68000(469) 37000(255) 25 30 1600(871...
Journal Articles
Alloy Digest (2015) 64 (10): SS-1228.
Published: 01 October 2015
... tensile properties, annealed bar Temperature, °C (°F) Ultimate tensile strength, MPa (ksi) Yield strength, MPa (ksi) Elongation, % 196 ( 320) 1489 (216) 820 (119) 36 73 ( 100) 938 (136) 545 (79) 51 Room temperature 717 (104) 372 (54) 55 204 (400) 579 (84) 221 (32) 52 427 (800) 524 (76) 186 (27) 50 538...
Journal Articles
Alloy Digest (2018) 67 (11): SS-1297.
Published: 01 November 2018
... cryogenic and elevated temperature tensile properties (annealed bar) 196 °C ( 320 °F) 1489 (216) 820 (119) 36 73 °C ( 100 °F) 938 (136) 545 (79) 51 Room temperature 717 (104) 372 (54) 55 204 °C (400 °F) 579 (84) 221 (32) 52 427 °C (800 °F) 524 (76) 186 (27) 50 538 °C (1000 °F) 476 (69) 165 (24) Physical...
Journal Articles
Alloy Digest (1992) 41 (8): SS-533.
Published: 01 August 1992
... 104.2 Type 304 B85 6.2 13.2 25.2 Colmonoy 6 C56 1.1 0.8 2.9 Armco l JlTRONIC 32 B95 4.2 4.3 7.1 Armca NTl-RoNIc 60 B95 2.8 2.3 *Crossed cylindas. 16 lbs (71 NJ 10,000 or 40.000 cycles, unlubricated, in air, room temperature, 37.9 13.5 2.2 6.8 corrected for density differences. Table 6 - CORROSIVE WEAR...
Journal Articles
Alloy Digest (2013) 62 (4): SS-1142.
Published: 01 April 2013
... tensile properties 196 °C ( 320 °F) 1579 (229) 1217 (176) 20 73 °C ( 100 °F) 1145 (166) 717 (104) 60 24 °C (75 °F) 807 (117) 496 (72) 49 93 °C (200 °F) 731 (106) 407 (59) 50 204 °C (400 °F) 641 (93) 310 (45) 44 538 °C (1000 °F) 510 (74) 221 (32) 39 Typical Charpy V-notch toughness Annealed bar 307 J...
Journal Articles
Alloy Digest (1976) 25 (1): SS-324.
Published: 01 January 1976
... % 68000 51 105000 32 140000 18 167000 10 181000 7.5 191000 6.5 19900n 5.0 Rockwell Hardness Tesr Tensile Yield Strength Elongarion Temperature Strength (0.2% Offset) (2 in.) oF psi osi % 0 10 20 30 40 50 60 115000 133000 160000 184000 200000 2 lOOO@ 3000 B95 c30 c37 c41 c42 c44 c45 0 142000 55000 64 -50...
Journal Articles
Alloy Digest (1998) 47 (6): SS-721.
Published: 01 June 1998
...(a) 48 152 SO(a) 29 50(a) 7 22 Table 8 Wear Compatibility of Self-Mated Austenitic Stainless Steels NW60 TjQe201 Type301 Typcm Nmonic 32 Nmnic 33 NW40 Nmnnic 50 Type310 Type316 Type= 95 90 90 90 95 94 93 99 72 91 iii 33 HRC 98 2.79 158 4.95 4.68 5.47 5.70 5.47 4.62 739 3.08 7.95 435 8.94 535 9.95...
Journal Articles
Alloy Digest (2002) 51 (1): SS-841.
Published: 01 January 2002
... 789/2507 (S32750) 800 116 550 80 15 32 A 789/2205 (S32205) 655 95 485 70 25 30.5 A 789/2205 (S31803) 620 90 450 65 25 30.5 A 789/19D (S32001) 620 90 450 65 25 30 A 249/316L (S31603) 485 70 170 25 35 90 A 249/304L (S30403) 485 70 170 25 35 90 Table 5 Comparison of the PRE Ranges for Various...
Journal Articles
Alloy Digest (1998) 47 (8): SS-727.
Published: 01 August 1998
... 67 165 24 60 60 427 800 434 63 159 23 58 64 538 law 421 61 159 23 57 64 649 1200 379 55 159 23 50 57 Anne&d.avcrageof4tesls Table 2 Stress Rupture Strength smrs Elma@amimsQamm MPa ksi liimhibe.b UilL lledeimotaraa,% 172 25 348 32 53 207 30 108 29 48 241 35 34 23 31 ~rstremperatuR649oC(1MO...
Journal Articles
Alloy Digest (1977) 26 (4): SS-338.
Published: 01 April 1977
... and taper must be properly machined to insure maximum service life. Machined surfaces of :he taper and keyways should have a surface finish of 32 RMS maximum. Improper machining can result in propeller wobble, crevices and sharp comers which can cause added bending stresses, potential crevice...
Journal Articles
Alloy Digest (1996) 45 (12): SS-663.
Published: 01 December 1996
... m sfm&ki(MR) .sIImgalui~~ ors4Lbm -4OVNi 60(415) 40 076) 20.0 Type409@aAsTMA240) 55 080) 25 (20505) 20.0 Nue:Anne&dsheessuip.andplate Table 3 Impact Strength SF-i-= Tmlper&uc A WCSkprudAE3 OF oc io.~lb/h* mm.N/md 39 0 136 152 13.405 2346 T- 32 0 109 122 10.722 1.876 LoIgmdd -25 -32 86 % 8.422 1.474...
Journal Articles
Alloy Digest (1976) 25 (8): SS-332.
Published: 01 August 1976
... should have a surface finish of 32 RMS maximum. Improper machining can result in propeller wobble, crevices and sharp comers which can cause added bending stresses, potential crevice corrosion problems, or stress raisers, all of which will result in premature failure. Roper size, shape and alignment of...