Crack Growth Rate Behavior of a Titanium-Aluminide Alloy During Isothermal and Nonisothermal ConditionsSource: Journal of Engineering Materials and Technology:;1995:;volume( 117 ):;issue: 001::page 118DOI: 10.1115/1.2804362Publisher: The American Society of Mechanical Engineers (ASME)
Abstract: Observations of isothermal fatigue, isothermal fatigue with superimposed load hold times, and thermomechanical fatigue (TMF) crack growth rate behavior of Ti-24Al-11Nb are presented and compared with results from previous studies on titanium and nickel-base superalloys. Elevated-temperature crack growth mechanisms in this alloy, which involve fatigue, oxidation and creep, and the influence of frequency, temperature, and hold-time are discussed. These mechanisms are used to interpret the observations of TMF crack growth. The limitations of current crack growth rate models based on the linear-elastic fracture mechanics parameter, K, are addressed.
keyword(s): Alloys , Fracture (Materials) , Titanium aluminide , Fatigue , Temperature , Mechanisms , Titanium , Nickel , Creep , Fracture mechanics , oxidation , Superalloys AND Stress ,
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| contributor author | J. J. Pernot | |
| contributor author | S. Mall | |
| contributor author | T. Nicholas | |
| date accessioned | 2017-05-08T23:47:24Z | |
| date available | 2017-05-08T23:47:24Z | |
| date copyright | January, 1995 | |
| date issued | 1995 | |
| identifier issn | 0094-4289 | |
| identifier other | JEMTA8-26969#118_1.pdf | |
| identifier uri | http://yetl.yabesh.ir/yetl/handle/yetl/115437 | |
| description abstract | Observations of isothermal fatigue, isothermal fatigue with superimposed load hold times, and thermomechanical fatigue (TMF) crack growth rate behavior of Ti-24Al-11Nb are presented and compared with results from previous studies on titanium and nickel-base superalloys. Elevated-temperature crack growth mechanisms in this alloy, which involve fatigue, oxidation and creep, and the influence of frequency, temperature, and hold-time are discussed. These mechanisms are used to interpret the observations of TMF crack growth. The limitations of current crack growth rate models based on the linear-elastic fracture mechanics parameter, K, are addressed. | |
| publisher | The American Society of Mechanical Engineers (ASME) | |
| title | Crack Growth Rate Behavior of a Titanium-Aluminide Alloy During Isothermal and Nonisothermal Conditions | |
| type | Journal Paper | |
| journal volume | 117 | |
| journal issue | 1 | |
| journal title | Journal of Engineering Materials and Technology | |
| identifier doi | 10.1115/1.2804362 | |
| journal fristpage | 118 | |
| journal lastpage | 126 | |
| identifier eissn | 1528-8889 | |
| keywords | Alloys | |
| keywords | Fracture (Materials) | |
| keywords | Titanium aluminide | |
| keywords | Fatigue | |
| keywords | Temperature | |
| keywords | Mechanisms | |
| keywords | Titanium | |
| keywords | Nickel | |
| keywords | Creep | |
| keywords | Fracture mechanics | |
| keywords | oxidation | |
| keywords | Superalloys AND Stress | |
| tree | Journal of Engineering Materials and Technology:;1995:;volume( 117 ):;issue: 001 | |
| contenttype | Fulltext |