1 |
Wheeler, O. E., "Spectrum Loading and Crack Growth", Trans. ASME, J. Basic Eng., Vol. D94, 1972, pp. 181-186.
|
2 |
Willenborg, J., Engle, R. M., and Wood, H. A., "A Crack Growth Retardation Model Using an Effective Stress Concept", AFFDL TM-71-1-FBR, 1971.
|
3 |
Elber, W., "The Significance of Fatigue Crack Closure. Damage Tolerance in Aircraft Structure", ASTM STP, Vol. 486, 1971.
|
4 |
Newman, J. C., "Advances in Fatigue Life Prediction Methodology for Metallic Material", NASA TM-107676, 1992.
|
5 |
Willson, D. G, The Design of High-Efficiency Turbomachinery and Gas Turbine, Fourth edition, MIT Press, 1989.
|
6 |
김경희, 김현재, 전승배, 김춘택, "스캘럽 형상을 가진 래디얼 터어빈 휠 균열진전 평가", 제1회 헬기심포지움, 2007.
|
7 |
Federal Aviation Administration Advisory Circular, AC-29.571, Fatigue Tolerance Evaluation of Metallic Structure, 2005.
|
8 |
Mercer, C., Soboyejo, A.B.O. and Soboyejo W.O., "Micromechanisms of Fatigue Crack Growth in a Forged Inconel 718 Nickel-Based Superalloy", Material Science and Engineering A, Vol. 270, Issue 2, 1999.
|
9 |
ABAQUS Theory Manual Ver. 6.9, SIMULIA Corp, 2009.
|
10 |
U.S. Department of Transportation, Federal Aviation Administration, DOT/FAA/AR-00/64, Turbine Rotor Material Design, 2000.
|
11 |
Department of Defense Handbook, MIL-HDBK-1783, Engine Structural Integrity Program(ENSIP), 1999.
|
12 |
Anderson, T. L., Fracture Mechanics: Fundamental and Applications, Third edition, CRC Press, 2005.
|
13 |
Bannantine, J. A., Comer, J. J., and Handrock, J. L., Fundamentals of Metal Fatigue Analysis, Prentice Hall, 1989.
|
14 |
Farmer, T. E., "Damage Tolerance Concept for Advanced Engine", AIAA, ASME, SAE and ASEE, Joint Propulsion Conference, 24th, AIAA-1988-3165, 1988, pp. 6-10.
|