Quantification of fastener-hole quality

Journal of Aircraft

Volumn 15, Issue 3, 1978, Pages 143-147

  Rudd, J L ^a,b   Gray, T D ^a,b  

^a AIR FORCE RESEARCH LABORATORY   (United States)

^b Structural Integrity Branch   (United States)

Author keywords

[No Author keywords available]

Indexed keywords

FASTENERS - FATIGUE; FRACTURE MECHANICS;

AIRCRAFT;

EID: 0017950727     PISSN: 00218669     EISSN: None     Source Type: Journal    
DOI: 10.2514/3.58332     Document Type: Article

References (10)

1. Wood, H. A., Gallagher, J. P., Engle, R. M., and Potter, J. M., “Current Practice on Estimating Crack Growth Damage Accumulation with Specific Application to Structural Safety, Durability and Reliability,” Air Force Flight Dynamics Laboratory, AFFDL-TR-75-32, Jan. 1976.
2. Anon., “Airplane Damage Tolerance Requirements,” Air Force Aeronautical Systems Division, MIL-A-83444, July 1974.
3. Anon., “Airplane Strength and Rigidity Reliability Requirements, Repeated Loads and Fatigue,” Air Force Aeronautical Systems Division, MIL-A-8866B, Aug. 1975.
4. Rudd, J. L. and Gray, T. D., “Equivalent Initial Quality Method,” Air Force Flight Dynamics Laboratory, AFFDL-TM-76-83-FBE, Sept. 1976.
5. Gran, R. J., Orazio, F. D., Paris, P. C., Irwin, G. R. and Hertzberg, R., “Investigation and Analysis Development of Early Life Aircraft Structural Failures,” Air Force Flight Dynamics Laboratory, AFFDL-TR-70-149, March 1971.
6. Pinckert, R. E., “Damage Tolerance Assessment of F-4 Aircraft,” A1AA-76-904, presented at AIAA Aircraft Systems & Technology Meeting, Dallas, Tex., Sept. 27-29, 1976.
7. Dumesnil, C. E., Gratke, S. D., Wilson, R. P., Martin, C. P., White, D. J. and Hooks, O. L., “A-7D ASIP Part I, Damage Tolerance and Fatigue Assessment Program,” Vought Corp., Rept. No. 2-53440/7R-5928, Vol. I, Jan. 1977.
8. Duval, R. E., “A-7A Fatigue Wing Crack Growth,” LTV Aerospace Corporation, Rept. No. 74-53452-172, Dec. 1974.
9. Gray, T. D., “An Equivalent Initial Flaw Analysis of the A-7A Wing Fatigue Test,” LTV Aerospace Corporation, Rept. No. 2-53410/ASIP/5DIR-10, May 1975.
10. Duval, R. E., “Fractographic Examination of A-7D ASIP Initial Quality Specimens,” LTV Aerospace Corp., Rept. No. 75-53452-078, June 1975.