P.R. Abelkis (1980).
“Effect of Transport Aircraft Wing Loads Spectrum Variation on Crack
Growth”. Effect of Load Spectrum Variables on Fatigue Crack Initiation and
Propagation.
D.F. Bryan and J.M. Potter (Eds.). ASTM STP 714, pp. 78-134. Also see AFFDL-TR-78-134 (1978, November).
ASTM, 2001 Annual Book of
Standards.
ASTM Subcritical Crack Growth Subcommittee E24.04 Internal
Minutes and Stress-Corrosion Cracking Round-Robin Documentation (1974-1975).
A.P. Berens and P.W. Hovey
(1981, December). “Evaluation of NDE
Reliability Characterization”.
AFWAL-TR-81-4160 (Vol. 1), Air Force Wright Aeronautical Laboratories.
R.G. Boeman (1991).
“Interlaminar Deformations on the Cylindrical Surface of a Hole in
Laminated Composites: An Experimental Study, Center for Composite Materials and
Structures Report 91-07”. Virginia
Polytechnic Institute and State University, Blacksburg, VA
T.R. Brussat, S.T. Chiu, and M. Creager (1977, December). “Flaw Growth in Complex Structures”. AFFDL-TR-77-79 (Vols. 1, 2 and 3), Air Force
Flight Dynamics Laboratory.
R.T. Bubsey, D.M. Fisher, M.H. Jones, and J.E. Srawley
(1973). “Compliance Measurements,
Chapter 4”. Experimental Techniques in Fracture Mechanics, 1. A.S. Kobayashi (Ed.). Society for Exp. Stress Analysis, pp. 76-95.
J.B. Chang, J.H. Stolpestad, M. Shinozuka, and R. Vaicaitis
(1978, March). “Improved Methods for
Predicting Spectrum Loading Effects – Phase I Report (Vols. 1 and 2). AFFDL-TR-79-3036, Air Force Flight Dynamics
Laboratory.
J.B. Chang (1981). “Round-Robin Crack Growth Predictions
on Center-Cracked Tension Specimens Under Random Spectrum Loading”. Methods
and Models for Predicting Fatigue Crack Growth Under Random Loading. J.B. Chang and C.M. Hudson (Eds.). ASTM STP 748, pp. 3-40.
J.B. Chang and C.M. Hudson (Eds.) (1981). “Methods and Models for Predicting Fatigue
Crack Growth Under Random Loading”.
ASTM STP 748.
J.B. Chang, R.M. Engle, and J. Stolpestad (1981). “ Fatigue
Crack Growth Behavior and Life Predictions for 2219-T851 Aluminum Subjected to
Variable-Amplitude Loadings”. Fracture Mechanics: Thirteenth Conference. R. Roberts (Ed.). ASTM STP 743, pp. 3-27.
M. Creager and A.W. Sommers (1977, November). “Development of a Crack Growth Rate Test for
Quality Control”. AFML-TR-77-193, Air
Force Materials Laboratory.
T.W. Crooker, S.J. Gill, G.R. Yoder, and F.D. Bogar (1982,
April). “Development of a Navy Standard
Test Method for Fatigue Crack Growth Rates in Marine Environments”. Presented at the ASTM Symposium on
Environment-Sensitive Fracture: Evaluation and Comparison of Test Methods, held
at the National Bureau of Standards, Gaithersburg, Maryland.
D.S. Dawicke and M.A. Sutton (1993, September). “Crack Tip Opening Angle Measurements and
Crack Tunneling Under Stable Tearing in Thin Sheet 2024-T3 Aluminum
Alloy”. NASA CR-191523.
D.S. Dawicke (1997).
“Residual Strength Predictions using a Crack Tip Opening Angle
Criterion”. Proceedings of the FAA-NASA Symposium on the Continued Airworthiness of
Aircraft Structures. DOT/FAA/AR-92/2,
pp.555-566.
D.S. Dawicke, J.C. Newman, Jr., J.H. Starnes, Jr., C.A. Rose,
R.D. Youn; and B.R. Seshadri (1999, September). “Residual Strength Analysis Methodology: Laboratory Coupons to
Structural Components”. Third Joint
FAA/DoD/NASA Conference on Aging Aircraft, Albuquerque, NM. http://techreports.larc.nasa.gov/ltrs/PDF/1999/mtg/NASA-99-3jcaa-dsd.pdf
H.D. Dill, C.R. Saff, and J.M. Potter (1980). “Effects of Fighter Attack Spectrum on Crack
Growth”. Effect of Load Spectrum Variables on Fatigue Crack Initiation and
Propagation.
D.F. Bryan and J.M. Potter (Eds.). ASTM
STP 714, pp. 205-217. Also see
AFFDL-TR-76-112 (1977, March).
P.R. Edwards, et al.
(1981, October). “Fatigue Test
Methodology”. AGARD-LS-118. North Atlantic Treaty Organization, Advisory
Group for Aerospace Research and Development.
J.S. Epstein and M.S. Dadkah (1993). “Moiré Interferometry in Fracture Research”. J.S. Epstein (Ed.). Experimental
Techniques in Fracture, pp. 427-508.
A.F. Grandt, Jr. and G.M. Sinclair (1972). “The Stress-Intensity Factors for Surface
Cracks in Bending”. Stress Analysis and Growth of Cracks Part 1,
ASTM STP 513, pp. 37-58.
A.F. Grandt, Jr. and T.D. Hinnerichs (1974, September). “Stress-Intensity Factor Measurements for
Flawed Fastener Holes”. Proceedings of the Army Symposium on Solid
Mechanics, 1974: The Role of Mechanics in Design – Structural Joints. AMMRC MC 74-8, Army Materials and Mechanics
Research Center, pp. 161-176.
S.J. Hudak, Jr., A. Sexena, R.J. Bucci, and R.C. Malcolm
(1978). "Development of Standard
Methods of Testing and Analyzing Fatigue Crack Growth Rate Data - Final
Report". AFML TR-78-40. Air Force Materials Laboratory,
Wright-Patterson Air Force Base, Ohio.
G.R. Irwin (1960, August).
“Plastic Zone Near a Crack and Fracture Toughness”. Proceedings
Seventh Sagamore Ordnance Materials Research Conference, MET E661-611/F.
L.A. James and W.E. Anderson (1969, April). “A Simple Experimental Procedure for Stress
Intensity Factor Calibration”. Journal of Engineering Fracture Mechanics
(Vol. 1), pp. 565-568.
JSSG-2006 (1998, October).
“Joint Service Specification Guide, Aircraft Structures”. Department of Defense.
H.W. Kiu and J.S. Ke (1975).
“Moiré Method, Chapter
4”. Experimental Techniques in Fracture Mechanics, 2. A.S. Kobayashi (Ed.). Society for Exp. Stress Analysis, pp.
111-165.
A.S. Kobayashi (1973).
“Photoelasticity Techniques, Chapter 6”. Experimental Techniques in
Fracture Mechanics, 1. A.S.
Kobayashi (Ed.). Society for Exp.
Stress Analysis, pp. 126-145.
G.E. Lambert and D.F. Bryan (1978, November). “The Influence of Fleet Variability on Crack
Growth Tracking Procedures for Transport/Bomber Aircraft”. AFFDL-TR-78-158, Air Force Flight Dynamics
Laboratory.
H. Liebowitz (1974, January).
“Fracture Mechanics of Aircraft Structures”. AGARD-AG-176, North Atlantic Treaty Organization, Advisory Group
for Aerospace Research and Development.
A.F. Liu and J.C. Ekvall
(1976). “Material Toughness and
Residual Strength of Damage Tolerant Aircraft Structure”. Damage
Tolerance in Aircraft Structures.
ASTM STP 486, pp. 98-121.
D.E. McCabe (Ed.) (1973).
“Fracture Toughness Evaluation by R-Curve Method”.
ASTM STP 527.
H. Mindlin and R.W. Landgraf (Eds.) (1976). “Use of Computers in the Fatigue
Laboratory”. ASTM STP 613.
D.H. Mollenhauer (1997).
“Interlaminar Deformation at a Hole in Laminated Composites: A Detailed Experimental Investigation Using
Moiré Interferometry”. Ph.D. Thesis,
Virginia Polytechnic Institute and State University, Blacksburg, VA.
D. Post, B. Han, and P. Ifju (2000). “Moiré Methods for Engineering and Science – Moiré Interferometry
and Shadow Moiré ”. P.K. Rastogi
(Ed.). Photomechanics, Topics Appl. Phys. 77, pp.151-196.
D.L. Potter (1982).
“Durability and Damage Tolerance Behavior of Adhesively Bonded Primary Structure”.
Design of Fatigue and Fracture
Resistant Structures. P.R. Abelkis
and C.M. Hudson (Eds.). ASTM STP 761, pp. 373-407.
P.K. Rastogi (Ed.) (2000).
“Photomechanics”. Topics Appl. Phys., 77.
J.L. Rudd, T.R. Brussat, S.T. Chiu, and M. Creager (1982). “Experimental Evaluation of Initial Flaw Criticality and Analysis Methods for Damage
Tolerant Air Force Aircraft”. Design of Fatigue and Fracture Resistant Structures. P.R. Abelkis and C.M. Hudson (Eds.). ASTM STP 761,
pp. 152-171.
C.R. Saff and M.S. Rosenfeld (1982). “Load-Environment Interaction Effects on Crack Growth in Landing
Gear Steel”. Design of Fatigue and Fracture Resistant Structures. P.R. Abelkis and C.M. Hudson (Eds.). ASTM STP 761, pp. 234-252.
D.A. Skinn, J.P. Gallagher, A.P. Berens, P.D. Huber, and J.
Smith (1994). Damage Tolerant Design
(Data) Handbook. WL-TR-94-4052.
Wright Laboratory, Air Force Materiel Command, Wright-Patterson Air
Force Base, Ohio.
C.W. Smith (1975). “Use
of Three-Dimensional Photoelasticity and Progress Related Areas, Chapter
1”. Experimental
Techniques in Fracture Mechanics, 2.
A.S. Kobayashi (Ed.). Society
for Exp. Stress Analysis, pp. 3-58.
T. Swift (1971).
“Development of the Fail-Safe Design Features of the DC-10”. Damage
Tolerance in Aircraft Structures.
ASTM STP 486, pp. 164-214.
T. Swift and D.Y. Wang (1970).
“Damage Tolerant Design-Analysis Methods and Test Verification of
Fuselage Structure”. Air Force Conference on Fatigue and Fracture,
1969. AFFDL-TR-70-144, Air Force Flight
Dynamics Laboratory, pp. 653-683.
TECH, Inc. (2001)
Website: www.techok.com
R.M. Verette, M.M. Ratwani, and D.P. Wilhem (1973, May; 1977,
August). “Development and Evaluation of
Methods of Plane Stress Fracture Analysis”.
AFFDL-TR-73-42, Air Force Flight Dynamics Laboratory, Part 1 and Part 2,
Vol. 1.
Vishay Measurements Group, Inc. (2001). Website: www.measurementsgroup.com
D.Y. Wang and D.E. McCabe (1976). “Investigation of R-Curve Using Comparative Tests with
Center-Cracked-Tension and Crack-Line-Wedge-Loaded Specimens”. Mechanics
of Crack Growth. ASTM STP 590, pp.
169-193.
R.P. Wei and S.R. Novak (1982, April). “Interlaboratory Evaluation of KIscc
Measurement Procedures for Steels – A Summary”. Presented at the ASTM Symposium on Environment-Sensitive
Fracture: Evaluation and Comparison of Test Methods, held at the National
Bureau
of Standards, Gaithersburg, Maryland.
J.T. Wozumi, T. Spamer, and G.E. Lambert (1980). “An Engineering Model for Assessing Load
Sequence Effects”. Effect of Load Spectrum Variables on Fatigue Crack Initiation and
Propagation. D.F. Bryan and J.M.
Potter (Eds.). ASTM STP 714, pp.
128-142.
G.R. Yoder, L.A. Cooley, and T.W. Crooker (1981). “Procedures for Precision Measurement of
Fatigue Crack Growth Rate Using Crack-Opening Displacement Techniques”. Fatigue
Crack Growth Measurement and Data Analysis. S.J.
Hudak, Jr. and R.J. Bucci (Eds.). ASTM
STP 738, pp. 85-102.