Halila, E. E., Lenahan, D. T. and Thomas, T. T., 1982, High Pressure Turbine Test Hardware Detailed Design Report, NASA CR-167955.
Mazur, Z., Hernandez-Rossette, A., Garcia-Illescas, R. and Luna-Ramirez, A., 2008, "Failure Analysis of a Gas Turbine Nozzle," Engineering Failure Analysis, Vol. 15, pp. 913-921.
Arkhipov, A. N., Krasnovskiy, Y. E. and Putchkov, I. V., 2011, "Probabilistic Life Assessment of Turbine Vanes," Proceeding of ASME Turbo Expo 2011, GT2011-45841.
Mazur, Z. and Perez-Hernandez, E. B., 2011, "Gas Turbine Nozzle Life Assessment due to Thermal Fatigue," Proceedings of ASME Turbo Expo 2011, GT2011-45247.
Zheng, X. Q., Du, T. and Zhang, Y. J., 2011, "Prediction of Thermal Fatigue Life of a Turbine Nozzle Guide Vane," Journal of Zhejiang University- Science A(Applied Physics & Engineering), Vol. 12, No. 3, pp. 214-222.
Huh, J. S., Rhee, D. H., Kang, Y. S., Seo, D. C. and Cha, B. J. 2014, "A Parametric Study on the High Pressure Turbine Nozzle of a Gas Turbine Engine for Structural Integrity," 8th China-Japan-Korea Joint Symposium on Optimization of Structural and Mechanical Systems, W2E_5_145.
Socie, D. F. and Marquis, G. B., 1999, Multiaxial fatigue, SAE, Int.
You, B. R. and Lee, S. B., 1996, "A Critical Review on Multiaxial Fatigue Assessments of Metals," International Journal of Fatigue, Vol. 18, No. 4, pp. 235-244.
Das, J. and Sivakumar, S. M., 2008, "Life Modeling of Notched CM247LC DS Nickel-Base Superalloy," Engineering Failure Analysis, Vol. 7, pp. 347-358.
Moore, Z. J., 2006, "Multiaxial Fatigue Life Prediction of a High Pressure Steam Turbine Rotor Using a Critical Plane Approach," Master thesis, Georgia Institute of Technology.
Kupkovits, P. A., 2008, "Thermomechanical Fatigue Behavior of the Directionally-Solidified Nickel-Base Superalloy CM247LC," Master Thesis, Georgia Institute of Technology.
Kang, Y. S., Rhee, D. H., Huh, J. S. and Cha, B. J., 2015, "Thermal Boundary Condition Effects on Conjugate Heat Transfer Analysis of High Pressure Turbine Nozzle," 2015 The 8th Asian-Pacific Conference on Aerospace Technology, 140223.
Military Handbook, 2002, "Engine Structural Integrity Program (ENSIP)," MIL-HDBK-1783B.