References
- Department of Defence Standard Practice, 2005, Aircraft Structural Integrity Program (ASIP), MIL-STD-1530C.
- Lee, D. and Achenbach, J. D., 2016, "Analysis of the Reliability of a Jet engine Compressor Rotor Blade Containing a Fatigue Crack," Journal of Applied Mechanics, Vol. 83, No. 4, p. 041004. https://doi.org/10.1115/1.4032376
- Gallager, J. P., Babish, C. A. and Malas, J. C., 2005, "Damage Tolerant Risk Analysis Techniques for Evaluating the Structural Integrity of Aircraft Structures," Proceedings of the 11th International Conference on fracture, Turin, Italy.
- Department of Defense Handbook, 2004, Nondestructive Evaluation System Reliability Assessment, MIL-HDBK-1823A.
- Li, M., Meeker, W. Q. and Hovey, P., 2011, "Joint Estimation of NDE Inspection Capability and Flawsize Distribution for In-service Aircraft Inspections," Statistics Preprints, p. 76.
- Singh, R., 2000, Three Decades of NDI Reliability Assessment, Report No. Karta-3510-99-01, Submitted to AF NDI Office.
- Thompson, R. B., 2008, "A Unified Approach to the Model-assisted Determination of Probability of Detection," Review of Quantitative Nondestructive Evaluation, Vol. 27, pp. 1685-1692.
- Lee, B. W., Suh, J., Lee, H. and Kim T. G., 2011, "Investigations on Fretting Fatigue in Aircraft Engine Compressor Blade," Eng. Failure Anal., Vol. 18, No. 7, pp. 1900-1908. https://doi.org/10.1016/j.engfailanal.2011.07.021
- Montgomery, D. C., 2012, Design and Analysis of Experiments, 8th ed., Wiley, Hoboken, NJ, pp. 523-530
- Satelli, A., Ratto, M., Andres, T., Campolongo, F., Cariboni, J., Gatelli. D., Saisana, M. and Tarantola, S., 2008, Global Sensitivity Analysis: The Primer, Wiley, Chichester, UK, pp. 155-167.
- Pawitan, Y., 2001, In All Likelihood, Oxford University Press, Oxford, UK, pp. 30-35.
- Tanner, M. A., 2012, Tools for Statistical Inference: Methods for the Exploration of Posterior Distributions and Likelihood Functions, Springer Science & Business Media, New York, p. 34.