Abstract

Fatigue crack growth testing under variable amplitude loading conditions is currently not standardized. Without standardization, the methods and techniques applied by different laboratories vary, and as such, lab-based bias can occur readily. The goal of this paper is to discuss in detail the experience developed and lessons learned during years of spectrum crack growth testing. Issues concerned with specimen geometry, crack geometry, precracking methodology, crack length measurement, spectrum content, load magnitude control, and interpretation of results are addressed herein. Although the ASTM Standard Test Method for Measurement of Fatigue Crack Growth Rates, E 647, provides guidance that is useful to this test, the specialized nature of spectrum testing does provide its own unique set of issues different from da/dN versus ΔK testing.

References

1.
Broek
,
D.
,
The Practical Use of Fracture Mechanics
,
Kluwer Academic Publishers, Dordrecht
,
The Netherlands
,
1989
.
2.
Lincoln
,
J. W.
, “
Damage Tolerance — USAF Experience
,”
Proceedings of the 13th Symposium of the International Committee on Aeronautical Fatigue
,
Pisa, Italy
,
1985
.
3.
Oberkampf
,
W. L.
, “
Methodology for Verification and Validation in Engineering Simulations
,” Presented at the
Symposium for Validation and Verification of Computational Mechanics Codes
,
California Institute of Technology
,
Pasadena, CA
,
12
1998
.
4.
Wheeler
,
O. E.
, “
Spectrum Loading and Crack Growth
,” Transactions of the ASME,
Journal of Basic Engineering
 0021-9223, Vol.
94
,
1972
, pp.
181
-
186
.
5.
Paris
,
P. C.
,
Tada
,
H.
, and
Donald
,
J. K.
, “
Service Load Fatigue Damage — A Historical Perspective
,”
International Journal of Fatigue
 0142-1123, Vol.
21
,
1999
, pp.
S35
-
S46
.
6.
Goranson
,
U. G.
, “
Fatigue Issues in Aircraft Maintenance and Repairs
,”
International Journal of Fatigue
 0142-1123, Vol.
19
, Supp. No.
1
,
1997
, pp.
S3
-
S21
.
7.
Damage Tolerance in Aircraft Structures
, ASTM STP 486,
ASTM International
,
West Conshohocken, PA
,
1971
.
8.
Fatigue Crack Growth Under Spectrum Loads
, ASTM STP 595,
R. P.
Wei
, Ed.,
ASTM International
,
West Conshohocken, PA
,
1976
.
9.
Service Fatigue Loads Monitoring, Simulation and Analysis
, ASTM STP 671,
P. R.
Abelkis
, Ed.,
ASTM International
,
West Conshohocken, PA
,
1979
.
10.
Effect of Load Spectrum Variables on Fatigue Crack Initiation and Propagation
, ASTM STP 714,
D. F.
Bryan
and
J. M.
Potter
, Eds.,
ASTM International
,
West Conshohocken, PA
,
1980
.
11.
Fatigue Rated Fastener Systems
,” AGARD Report No. 721,
H. H.
VanDerLinden
, Ed.,
North Atlantic Treaty Organization
, Advisory Group for Aerospace Research and Development,
1985
.
12.
McKeighan
,
P. C.
and
Smith
,
D. J.
, “
Determining the Potential Drop Calibration of a Fatigue Crack Growth Specimen Subject to Limited Experimental Observations
,”
Journal of Testing and Evaluation
 0090-3973, Vol.
22
, No.
4
,
07
1994
, pp.
291
-
301
.
13.
Dwyer
,
W.
, “
Development of a Supplemental Inspection Document for the Fairchild SA226 and SA227 Aircraft
,” Part 2, Vol.
II
,
Appendix F-Testing and Analysis for DTA of Fairchild SA226 Main Wing Spar Lower Cap at WS99
, DOT/FAA/AR-99/20, P2, Vol.
II
,
10
1999
.
14.
Schijve
,
J.
,
Fatigue of Structures and Materials
,
Kluwer Academic Publishers
,
2001
.
15.
Piascik
,
R. S.
and
Willard
,
S. A.
, “
The Characteristics of Fatigue Damage in the Fuselage Riveted Lap Splice Joint
,” NASA/TP-97-206257,
NASA Langley Research Center
,
Hampton, VA
,
1997
.
16.
GENESIS 4 Fatigue CD: GENErate StandardIsed Sequences
,”
National Aerospace Laboratory (NLR)
,
Loads and Fatigue Department
,
Emmeloord, The Netherlands
,
2001
.
17.
McKeighan
,
P. C.
,
Fess
,
F. E.
 II
,
Petit
,
M.
, and
Campbell
,
F. S.
, “
Quantifying the magnitude and Effect of Loading Errors During Fatigue Crack Growth Testing Under Constant and Variable Amplitude Loading
,”
Applications of Automation Technology in Fatigue and Fracture Testing and Analysis: Fourth Volume
, ASTM STP 1411,
A. A.
Braun
,
P. C.
McKeighan
,
A. M.
Nicolson
, and
R. D.
Lohr
, Eds.,
ASTM International
,
West Conshohocken, PA
,
2002
.
18.
Donald
,
K. J.
and
George
,
K.
, “
Variable Amplitude Fatigue Crack Growth Using Digital Signal Processing Technology
,”
Symposium on Fatigue Testing and Analysis Under Variable Amplitude Loading
, ASTM STP 1439,
P. C.
McKeighan
and
N.
Ranganathan
, Eds.,
ASTM International
,
West Conshohocken, PA
,
2003
.
19.
Virkler
,
D. A.
,
Hillberry
,
B. M.
, and
Goel
,
P. K.
, “
The Statistical Nature of Fatigue Crack Propagation
,” Transactions of the ASME,
Journal of Engineering Materials and Technology
 0094-4289, Vol.
101
,
1979
, pp.
148
-
153
.
This content is only available via PDF.
You do not currently have access to this content.