Titanium alloys and processing for high speed aircraft

Materials Science and Engineering: A

Volumn 243, Issue 1-2, 1998, Pages 299-304

  Brewer, William D ^a   Bird, R Keith ^a   Wallace, Terryl A ^a  

^a NASA LANGLEY RESEARCH CENTER   (United States)

Author keywords

Processing techniques; Research; Ti alloys

Indexed keywords

AIRCRAFT MATERIALS; HEAT TREATMENT; INDUSTRIAL RESEARCH; SUPERPLASTICITY; TENSILE STRENGTH; THERMAL EFFECTS; TITANIUM SHEET; TOUGHNESS;

HIGH SPEED AIRCRAFT;

TITANIUM ALLOYS;

EID: 0032025469     PISSN: 09215093     EISSN: None     Source Type: Journal    
DOI: 10.1016/s0921-5093(97)00818-6     Document Type: Article

References (6)

1. P.L. Martin, Toughness-strength trend in alloys derived from Ti-4.5Al-5Mo-1.5Cr, Proc. 8th World Conf. on Titanium. Birmingham, England, 1995, pp. 940-947.
2. ASTM E1152-87, Standard test method for determining J-R curves, 1992 Annual Book of ASTM Standards, vol. 03.01, ASTM, Philadelphia, PA, 1992, pp. 847-857.
3. ASTM E466-82, Standard test method for J1C, a measure of fracture toughness, 1992 Annual Book of ASTM Standards, vol. 03.01, ASTM, Philadelphia, PA, 1992, pp 732-746.
4. R.W. Hertzberg, Deformation and Fracture Mechanics of Engineering Materials, Wiley, New York, 1983.
5. R.K. Bird, T.A. Wallace, W.D. Brewer, Effects of heat treatment on microstructure, strength and toughness of Timetal 21S, Proc. 125th TMS Annual Meeting, Warrendale, PA, 1996, pp. 473-480.
6. J. Hatakeyama, Aerospace Eng. 15 (1995) 25-29.