High cycle fatigue behavior of Ti-6Al-4V with simulated foreign object damage

Mechanics of Materials

Volumn 33, Issue 11, 2001, Pages 679-692

  Mall, Shankar ^a,c   Hamrick II, Joseph L ^b   Nicholas, Theodore ^a  

^a AIR FORCE RESEARCH LABORATORY   (United States)

^b USAF   (United States)

^c AIR FORCE INSTITUTE OF TECHNOLOGY   (United States)

Author keywords

[No Author keywords available]

Indexed keywords

DEFORMATION; FATIGUE OF MATERIALS; FATIGUE TESTING; FINITE ELEMENT METHOD; RESIDUAL STRESSES; SHEAR STRESS; STRENGTH OF MATERIALS;

FOREIGN OBJECT DAMAGE (FOD);

TITANIUM ALLOYS;

EID: 0035498456     PISSN: 01676636     EISSN: None     Source Type: Journal    
DOI: 10.1016/S0167-6636(01)00084-9     Document Type: Article

References (14)

1. Understanding and preventing failures and their causes in gas turbine engines
2. High cycle fatigue in aircraft gas turbines - An industry perspective
3. Navy foreign object damage and its impact on future gas turbine low pressure compression system
4. Effects of ballistic impact damage on fatigue crack initiation in Ti-6Al-4V simulated engine blades
5. A rapid method for generation of a Haigh diagram for high cycle fatigue
6. Critical issues in high cycle fatigue
7. Influence of foreign-object on crack initiation and early crack growth during high-cycle fatigue of Ti-6Al-4V
8. Role of foreign object damage on thresholds for high-cycle fatigue in Ti-6Al-4V
9. Influence of foreign object damage (FOD) on fatigue life of simulated Ti-6Al-4V airfoils
10. Erosion, corrosion and foreign object damage in gas turbines
11. The foreign object damage project of the PRDA V HCF materials and life methods program
12. The effect and assessment of foreign object damage to aero engine blades and vanes