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Virgo 39

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Journal Articles
Alloy Digest (2004) 53 (8): SS-905.
Published: 01 August 2004
... Virgo 39 is a 1% Mo low-carbon martensitic stainless steel. This composition allows both weldability and enhanced corrosion resistance. The alloy is primarily designed for erosion-corrosion resistance in Pelton wheel and Kaplan blade-type applications. This datasheet provides information on...
Journal Articles
Alloy Digest (2013) 62 (5): SS-1145.
Published: 01 May 2013
... Virgo 17.4 PH is a 17Cr-4Ni-3Cu-0.3% Cb alloy that is precipitation hardening. It is martensitic and combines high mechanical properties with corrosion resistance. This datasheet provides information on composition, physical properties, hardness, elasticity, and tensile properties as well as...
Journal Articles
Alloy Digest (1968) 17 (12): Ni-141.
Published: 01 December 1968
... Hear treated 53-56 34-38 22.0-30.0 (Hardness at room remperarvre Rc 32-39) 5.7-7.3 9.7-11.0 8.2-9.9 16.0 8.2-9.5 26.0-37.0 Table 2 - TYPICAL WROUGHT PROPERTIES - Forged Bar Test TenSlIe Yield Reduction Temperature Srrcqrh Strength Elonpxion 01 ,Arc3 F Condirnon ksi R,, ,!1.2- I . in 2 c - - - - R.T...
Journal Articles
Alloy Digest (1954) 3 (5): Ni-10.
Published: 01 May 1954
... gsJ= 030 Tablo 1 TYPICAL PROPERnEs 0.85 03s Axmkd Nom&d =w almolium 0.70 Nkkd 0.5s Tensikstrenerh. psi 102000 143000 135Oocl Molyb&lllm 0.10 Yiddtpenertspi ssooo LOO000 120000 vanadium 0.10 ElW%hin' 22 14 18 Boron Raiuctiollafuq% 48 39 SO lral Bkdl- 201 293 275 Tauo2TYPKALHEATTREmED pB0PEKTIEs (1...
Journal Articles
Alloy Digest (1960) 9 (6): Ni-58.
Published: 01 June 1960
... 133,800 76,500 32 800 123,800 73,000 40 1000 125,000 76,000 39 1200 118,000 78,500 26 1350 95,000 68,200 18 1500 59,000 46.000 24 1600 38,200 27,800 50 DOI: 10.31399/asm.ad.ni0058 Copyright © ASM International® 1996 Heat Treatment: Solution Anneal - Heat at 1950 to 2000°F for 20 min. to 1 hour followed...
Journal Articles
Alloy Digest (1969) 18 (12): Ni-149.
Published: 01 December 1969
... 5 :x 30 40 i8 70 Vickers Hardness Number approx. 140 170 200 250 275 290 310 315 320 Test Temperature oF 600 800 1000 1200 1400 1600 1800 Tensile Strength psi 90500 88500 84000 65000 27500 15000 7500 Yield Strength Elongation psi (0.2%) % in 2 in. 31000 46 29500 49 28500 47 26500 39 17000 46 9oo J...
Journal Articles
Alloy Digest (1965) 14 (2): Ni-98.
Published: 01 February 1965
... mtrmpdb, psi 173900- 196500 Yiel& ruen~th. psi (0.2%) 112500-145!?00 Elongation, % iu 4D 22.7-27.4 Reducrion of area, x 23.2-48.3 Rockacll hnrdneas (x3-39 Tabi. 2 - TYPICAL ELEYATED TEMPERATURE PROPERTIES (Heated 1625oP for 24 hrr.. sir cooled, r&cared 1300°F for 20 lus.. air cooled) 8.30 0.300 2540-2600...
Journal Articles
Alloy Digest (1965) 14 (4): Ni-100.
Published: 01 April 1965
... 133800 76500 32 800 123800 ;3000 40 1000 125000 ;6000 39 1200 118000 78500 26 1350 75000 68200 18 1500 57000 46000 24 1600 38XlO 2 800 50 Table 3 - TYPICAL STRESS-RUPTURE DATA - Bars (Solurion Annealed 1775oF/4 hrs. Plus Aged 13OOoF 20 hrs.) Test Temperarure Srress, psi, to produce rupture in oF 100 Hrs...
Journal Articles
Alloy Digest (1961) 10 (12): Ni-6.
Published: 01 December 1961
... 76000 58000 39 26 2 20 15 3 8' a ~-we-- T 650 700 750 815 100 hrs. 69500 53800 38100 22400 TaMo 2 CREEP STRENGTH (Fully Heat-Treated) Stress, psi to produce extension of:- 0.1% in 0.2% in. 300 1000 5000 100 300 1000 hrs. hKS. tlrs. tlrs. Ill-s. hrs. 65000 58200 50400 73900 68300 61600 48200 42600 35800...