Accession Number : AD0747207
Title : Heat Treatment Study of Beta Extruded Titanium Alloy Ti-6Al-6V-2Sn.
Descriptive Note : Technical rept. Apr-Dec 71,
Corporate Author : AIR FORCE MATERIALS LAB WRIGHT-PATTERSON AFB OHIO
Personal Author(s) : Sajdak,R. J. ; Geisendorfer,R. F. ; Hall,J. A. ; Pierce,C. M.
Report Date : JUN 1972
Pagination or Media Count : 25
Abstract : A linear regression analysis was used to analyze mechanical property data from a statistically designed experiment which maximized the variability in heat treating parameters of a titanium alloy, Ti-6Al-6V-2Sn, beta extruded ribbed panel. Using the results of the linear regression analysis, a computer program was executed to predict mechanical properties. Nine heat treatment cycles were chosen to test the validity of the predicted mechanical properties. Generally, the yield strength and ultimate strength are slightly higher than predicted; reduction of area is about as predicted; elongation is slightly lower than predicted; and fracture toughness is lower than predicted. Two heat treatment cycles were singled out as yielding superior properties over the other heat treatment cycles investigated. (Author)
Descriptors : (*TITANIUM ALLOYS, HEAT TREATMENT), REGRESSION ANALYSIS, MICROSTRUCTURE, MECHANICAL PROPERTIES, ALUMINUM ALLOYS, VANADIUM ALLOYS, TIN ALLOYS
Subject Categories : Properties of Metals and Alloys
Distribution Statement : APPROVED FOR PUBLIC RELEASE