1966
DOI: 10.6028/jres.070c.003
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Effect of temperature and notch geometry on the tensile behavior of a titanium alloy

Abstract: A comprehensive study was made of the effec ts of notc h geometry on the mec hanical behavior of a duplex-annealed titanium-8 aluminum-1 molybdenum-1 vanadium all oy within th e te mperature range 75 to 1200 of (297 to 921 O K). Yi eld strength , tensile strength , and true stress at fracture increased with increase in notc h depth and decrease in notch angle and te mperature. The maximum strength (tensile and yield) properties were obtained for the cylindrical specim ens having a root radiu s of O.OI -inch. G… Show more

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Cited by 6 publications
(10 citation statements)
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“…16 at the nominal stresses of 50 and 500 MPa. The peak value of 11 Optical micrograph taken at unfractured notch section at 298 K: notch root radius is 0?5 mm Triaxiality factor (TF) is defined as the ratio of hydrostatic stress to Von Mises equivalent stress and is given as TF~(s 1 zs 2 zs 3 )=3s eq (5) It is the indicator of degree of constraint imposed by the notch by means of developing triaxial stress state in the notch region. 17,18 The variations of triaxiality factor across the notch section at the nominal stresses of 50 and 500 MPa are shown for various notch radii in Fig.…”
Section: Fea Resultsmentioning
confidence: 99%
See 1 more Smart Citation
“…16 at the nominal stresses of 50 and 500 MPa. The peak value of 11 Optical micrograph taken at unfractured notch section at 298 K: notch root radius is 0?5 mm Triaxiality factor (TF) is defined as the ratio of hydrostatic stress to Von Mises equivalent stress and is given as TF~(s 1 zs 2 zs 3 )=3s eq (5) It is the indicator of degree of constraint imposed by the notch by means of developing triaxial stress state in the notch region. 17,18 The variations of triaxiality factor across the notch section at the nominal stresses of 50 and 500 MPa are shown for various notch radii in Fig.…”
Section: Fea Resultsmentioning
confidence: 99%
“…Yield strength, tensile strength and true stress at fracture of a duplex annealed Ti8Al1Mo1V alloy increased with increase in notch depth and decrease in notch angle. 5 Toribio 6 used two notches with different radii to analyse the influence of the stress state in the vicinity of the notch tip on hydrogen embrittlement.…”
Section: Introductionmentioning
confidence: 99%
“…This alloy was selected for th e research as it is one of the candida te materials for aerospace applications in components used at intermedi ate tempera tures (up to 1000 OF ) . Furthermore, its shorttime tensile notch behavior a nd lon g-time creep properti es on unnotched cylindri cal specimens have been ex tensively investigated at the National Bureau of Standards [3,6] .…”
Section: Material Specimens and Experimental Proceduresmentioning
confidence: 99%
“…The test specimens we re pre pared from bars obtained from the same heat as that used in a previous researc h program to evaluate the effects of notch geometry on the tensile behavior of this alloy [3]. The bars were cut into lengths , each about 6.5-in and annealed at 1750 O F (1226 OK) for 1 hr and aircooled.…”
Section: Materials and Testing Proceduresmentioning
confidence: 99%
“…= rupture tim e (2) (2a) cr = creep s tress n, nl , A, S , A I, a nd BI = co ns tant s whic h are d e pe nde nt on te mpera ture. ~s = A exp (Bcr) (3) a nd (3a)…”
Section: Extension-time Relations For Specimens Tested At 1200 Ofmentioning
confidence: 99%