[
[1] Beattie, A., Dahlke, L., Gieske J., Hansche B., Phipps, G., Roach D., Shagam R. and Thompson K., 1994, “Emerging Nondestructive Inspection Methods for Aging Aircraft – Final Report”, DOT/FAA/CT-94/31, Federal Aviation Administration, Atlantic City International Airport, N.J.10.2172/10136510
]Search in Google Scholar
[
[2] Goranson, U., 1997, “Fatigue issues in aircraft maintenance and Repairs”, Int. J. Fatigue, 20(6), pp. 413-431.10.1016/S0142-1123(97)00029-7
]Search in Google Scholar
[
[3] Ostash, O., Fedirko, V., Uchanin, V. Bychkov, S., Moliar O., Semenets, O., Kravets V., Derecha V., 2007, Fracture mechanics and strength of materials, Vol. 5. Strength and durability of airplane materials and structural elements (in Ukrainian), Lviv, Spolom.
]Search in Google Scholar
[
[4] McMaster, R.C., and McIntire, P., Mester, M.L., Eds, 1986, Nondestructive testing handbook (second edition), Vol. 4, Electromagnetic testing, American Society for NDT.
]Search in Google Scholar
[
[5] Udpa, S.S., More P.O., Eds, 2004, Nondestructive testing handbook (third edition), Vol. 5, Electromagnetic testing, American Society for NDT.
]Search in Google Scholar
[
[6] Uchanin, V., 2006, “Eddy current methods for detection of the defects in rivet areas of multilayer aircraft structures” (in Russian), Technical diagnostics and nondestructive testing, 3, pp. 3-12.
]Search in Google Scholar
[
[7] Sasi, B., Rao, B.P.C., Jayakumar, T. and Baldev Raj, 2009, “Development of Eddy Current Test Procedure for Non-destructive Detection of Fatigue Cracks and Corrosion in Rivets of Air-intake Structures”, Defence Science Journal, 59(2), pp. 106-112.10.14429/dsj.59.1497
]Search in Google Scholar
[
[8] Mohd Ali, Imran Hussin and Md Hairudin, 2019, “Defect Analysis on Boeing 737-400 Skin Panel Rivet Row Aft Ward Fuselage” Int. J. Innovative Technology and Exploring Engineering, 8(6S).
]Search in Google Scholar
[
[9] Harrison, D.J., 1984, ”Detection of surface cracks near a workpiece fastener hole by means of a rotatable probe”, U.S. Patent 4445089.
]Search in Google Scholar
[
[10] Harrison, D.J., 1985, ”Eddy current measurement apparatus for non-destructive testing in the vicinity of fastener”, U.S. Patent 4496904.
]Search in Google Scholar
[
[11] Harrison, D.J., 1994, Method and apparatus for non-destructive testing of electrically conductive materials, U.S. Patent 5298858.
]Search in Google Scholar
[
[12] Harrison, D.J., 1987, “The Detection of Cracks under Installed Aircraft Fasteners by Means of a Scanning Eddy-Current Method”, Review of Progress in Quantitative Nondestructive Evaluation, eds. D.Thompson and D. Chimenti, Vol. 6A, pp. 1013-1017.10.1007/978-1-4613-1893-4_116
]Search in Google Scholar
[
[13] Sheppard, W., Tam, K., 1995, ”Eddy current probe having body of high permeability supporting drive coil and plural sensors”, U.S. Patent 5399968.
]Search in Google Scholar
[
[14] Hurley, D., Gilmore, R., Young, J., 1996, ”Eddy current surface inspection probe for aircraft fastener inspection, and inspection method”, U.S. Patent 5510709.
]Search in Google Scholar
[
[15] Arnaud, J., Floret, M., 1984, ”Process and device for the detection of cracks in riveted joints using an eddy current probe”, U.S. Patent 4677379.
]Search in Google Scholar
[
[16] Uchanin, V., 2013, Surface double differential type eddy current probes (in Ukrainian), Spolom, Lviv.
]Search in Google Scholar
[
[17] Mook, G., Hesse, O., Uchanin, V., 2007, “Deep penetrating eddy currents and probes”, Materials Testing, 49(5), pp. 258-264.10.3139/120.100810
]Search in Google Scholar
[
[18] Uchanin, V., Mook, G., Stepinski, T., 2002, “The investigation of deep penetrating high resolution EC probes for subsurface flaw detection and sizing”, Proc. 8-th Europ. Conf. for Nondestructive Testing. 2002. Barcelona. (www.ndt.net).
]Search in Google Scholar
[
[19] Uchanin, V., Nardoni, G., 2019, “Detection of cracks in ferrous steel structures: new innovative eddy current techniques”, Procedia Structural Integrity (ESIS), 16, pp. 198-204.10.1016/j.prostr.2019.07.041
]Search in Google Scholar
| Jul 24, 2020