Spectrum loading and crack growth

Journal of Fluids Engineering, Transactions of the ASME

Volumn 94, Issue 1, 1972, Pages 181-186

  Wheeler, O E ^a  

^a GENERAL DYNAMICS   (United States)

Author keywords

[No Author keywords available]

Indexed keywords

MATHEMATICAL INSTRUMENTS;

CRACK GROWTH;

METALS AND ALLOYS--FATIGUE;

EID: 0015316080     PISSN: 00982202     EISSN: 1528901X     Source Type: Journal    
DOI: 10.1115/1.3425362     Document Type: Article

References (16)

1. Schijve, J., “Fatigue Crack Propagation in Light Alloy Sheet Material and Structures,” Advances in Aeronautical Sciences, Pergamon Press, New York, N. Y., 1961, pp. 387-408.
2. Hudson, C. M., and Hardrath, H. F., “Effects of Changing Stress Amplitude on the Rate of Fatigue Crack Propagation in Two Aluminum Alloys,” NAS TN-D 960, Sept. 1961.
3. Hudson, C. M., and Hardrath, H. F., “Effects of Variable. Amplitude Loadings on Fatigue Crack Propagation Patterns,” NAS TN-D 1803, Aug. 1963.
4. Schijve, J., Jacobs, F. A., and Tromp, P. J., “Crack Propagation in Aluminum Alloy Sheet Materials Under Flight-Simuiation Loading,” NL TR 68117 U (AD 692467), Dec. 1968.
5. Paris, P. C., “The Growth of Cracks Due to Variations in Load,” PhD dissertation, Lehigh University, 1962.
6. Smith, S. H., “Random-Loading Fatigue Crack Growth Behavior of Some Aluminum and Titanium Alloys,” Structural Fatigue in Aircraft, ASTM Special Technical Publication No. 404, Philadelphia, Pa., 1966, pp. 74-100.
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9. Forman, R. G., Kearney, V. E., and Engle, R. M., “Numerical Analysis of Crack Propagation in Cyclic-Loaded Structures” JOURNAL OF BASIC ENGINEERING, TRANS. ASME, Series D, Vol. 89, 1967, pp. 459-464.
10. Miner, M. A., “Cumulative Damage in Fatigue,” Journal of Applied Mechanics, Vol. 12, TRANS. ASME, Vol. 67, 1945, pp. A-159-A-164.
11. Williams, M. L., “On the Stress Distribution at the Base of a Stationary Crack,” Journal of Applied Mechanics, Vol. 24, TRANS. ASME, Vol. 79, Series E, No. 1, Mar. 1957, pp. 109-114.
12. Irwin, G. R., “The Crack Extension Force for a Part Through Crack in a Plate,” Journal of Applied Mechanics, Vol. 29, TRANS. ASME, Vol. 84, Series E, No. 3, Sept. 1962, pp. 651-654.
13. “Proposed Method of Test for Plane Strain Fracturc Toughness of Metallic Materials,” ASTM Standards Test Method 14339, 1970.
14. Masters, J. N., Haese, W. P., and Finger, R. W., “Investigation of Deep Flaws in Thin Walled Tanks,” NASA CR-72600, Dec., 1969.
15. “F-lll Wing Carry-Through Box Assembly Feasibility Study,” General Dynamics Corporation Report FZM-12-10732-11, Fort Worth, Texas, 27 June 1969, pp. 32-37.
16. Simodynes, E. E., “Cycle by Cycle Simulation of Fatigue Crack Growth for Spectrum Loading,” General Dynamics Corporation Report MRL-127, Fort Worth, Texas, 15 June 1970.