1. Advisory Circular 33.14-1. Damage tolerance for high energy turbine engine rotors,2001
2. Advisory Circular 33.70-1. Guidance material for aircraft engine-life-limited parts requirements,2009
3. Fu D B, Tao Z, Zhang G, et al. Safety evaluation of cooling configuration in a rotor-stator cavity. Proceedings of 2009 International Symposium on Aircraft Airworthiness, 2009; 376-381.
4. CFR 14 part 33. Airworthiness standards: aircraft engines,2009
5. Prediction of heat transfer in a rotating cavity with a radial outflow;Ong;Journal of Turbomachinery,1991